[14:51:35] NASSP Logging has been started by n7275 [14:51:37] hello [14:52:57] hey Matt [14:59:12] any reason why we can't close the cabin fan GitHub issue? it seems to be resolved [15:00:45] I think so. What got implemented isn't exactly what Thymo was suggesting, but the solution does the same, more acceptable volume. [15:09:23] okay. I think we are going to need to revisit sound in general if we want to consider migrating to the next version of Orbiter [15:11:39] yes [15:23:04] ok, put all my current RTCC work on Github [15:23:19] just needs testing and maybe more documentation [16:04:40] on the subject of countdown holds, would it be easier to just add a new time variable, rather than trying to change/remove all the instances of mission time? [16:29:27] yeah I think that is the way to go. in a lot of places the mission time is mostly used as a regular time interval even with saving/loading [16:29:53] the main challenge will be the prelaunch sequence of events in satsystems, mostly for the ECS [16:30:08] a lot of that codes belongs in the mobile launcher somewhere [16:30:11] code* [16:34:06] speaking of plans that haven't come to fruition yet, a while ago I wanted to write an Apollo 12 specific RTCC MFD guide, but I guess you need to fly without that for now... [16:35:29] morning! [16:36:50] hey Mike [16:37:03] how is the CDU doing [16:37:25] I'm down to only 12 nets with errors for tray X in the backplane viewer [16:37:37] although resolving the nets has raised a lot of questions that need to be beeped out [16:38:14] ....and this is only for LM backplanes. I'm sure it will be a disaster again if I try to generate a CSM one [16:38:58] yeah this CSM/LM mixture seems to get in the way a bit :D [16:40:00] it wouldn't be so bad if they annotated their schematics consistently [16:41:07] like two pins almost right next to each other in the schematic. one of them is clearly marked as only connected in the LM, the other is not [16:41:17] but they're both only connected in the LM, and they are separated by a pin that's connected in both vehicles [16:41:20] not helpful, MIT [16:44:43] yeah that's quite annoying [16:50:06] the one I'm stuck on now is the IMU cage signal, which is put out on pins 109 and 110 [16:50:29] both unmarked implying always connected for all axes, which is clearly false [16:50:46] but also both are explicitly marked as going to the mode module [16:50:59] but it seems like only the pin 109 signal ever actually makes it there [16:51:11] so I don't know if pin 110 is just unwired or what [16:56:41] CDU outputs IMU cage command? [16:57:25] something like that [16:57:38] at least it's a signal called CAGE [17:00:06] I'm seeing some signal going to the IMU, looks like 1x sine and cosine input from IMU is send back to the IMU to drive it to zero when you cage it [17:00:20] oh, not sure if it's useful at all to you, but I have the SA-502 version of https://www.ibiblio.org/apollo/Documents/UAH-19671205-InterfaceControlDocumentDefinitionOfSaturnSA507FlightSequenceProgram.pdf arriving today [17:00:23] ah yeah that'll be it [17:00:48] oh nice, Apollo 6, yes that could be useful [17:02:06] I do already have the S-IVB stage flight test plan for that mission [17:02:42] nice :D [17:02:58] which has most if the flight sequence program, but there are a bunch of TBDs [17:03:03] so might be an early version [17:03:07] of* [17:03:35] so good to have something more official :D [17:04:37] oh and the S-IVB flight evaluation report also has all of the events [17:04:54] but still, it's good to cross check. And there might some sequences not used on the actual mission [17:07:25] and what mode module is that? Also part of the CDU, right? [17:08:08] just from the Systems Handbook the CAGE signal is always connected to the three gyro servo amplifier relay module, part of the IMU [17:08:15] and that has cage and coarse align relays [17:08:23] which would allow that cage signal to do something [17:10:21] oh god the IMU wiring there is complex :D [17:10:25] hahahaha [17:10:30] yeah the mode module is part of the CDU [17:10:55] but it's mostly the IMU cage switch that gives the cage signal to the IMU [17:11:25] there is a second path, looks maybe like during IMU turn-on it also has it caged still [17:11:47] and also my sleepy brain was conflating the CAGE signals, which I also had problems with, with the other signals that I actually got stuck on: _CSRFH and _CSRFL [17:12:15] which are the cosine(theta-psi) reference from the quadrant select modules and definitely CDU-internal [17:29:55] yeah the CSM CDU backplane is going to be a complete bloodbath when I delete the optics coarse modules [17:30:35] it's almost too bad that I don't have access to a CSM CDU tray X to see if they still had any wires connected there at all [17:43:20] what's better than owning one CDU. Owning two CDUs! [17:44:10] just steal a whole CM from some museum, how hard can it be [18:06:55] hahahaha [18:07:21] I don't know if I want two CDUs [18:07:30] one is radioactive enough [18:13:53] haha right [18:15:04] and what's the rope reader doing? Getting as much attention as the CDU? [18:17:45] aluminum parts are in https://photos.app.goo.gl/BD72o1X51yZqBgKw6 [18:17:55] the test backplane board is allegedly being delivered today [18:18:04] and I started doing the layout for the full driver board last night [18:18:32] it hasn't been getting as much, but I'm going to start focusing on it almost exclusively again until the driver board layout is done [18:19:42] if the backplane fits I'm going to take over the rear aluminum plate to Marc's so we can install all of the female Samtec/Malco pins [18:29:04] they are already experts at AGC pins [18:31:46] yep! [19:51:45] ah! backplane boards are here [19:51:50] let's see if this all fits together [20:03:08] yesss it works :D [20:08:49] :D [20:11:08] I don't think any changes are necessary outside of actually routing all of the connections on it [20:11:20] the driver board plugs into it just fine [20:11:38] malco pin holes are well-aligned with the mounting holes on the rear plate [20:12:24] the orientation of the rope module pins is correct [20:18:26] https://photos.app.goo.gl/71LVreEXaLUGbwD5A [20:18:50] https://photos.app.goo.gl/g3T1sivEngcQNQwL6 [20:19:59] beautiful [21:04:16] night! [14:21:38] good afternoon [14:40:24] hey [14:43:24] what's the latest on your CSM exterior lighting PR? Was there anything left to do? [15:45:08] I think it can be merged [15:45:21] I was just waiting on feedback in the visuals [16:03:31] there are more lights to add (running and eva) but that requires mesh work and I have no idea what I'm doing there [16:19:34] hmm [16:19:41] RndzLightSwitch.refresh(simdt); [16:19:47] I feel like this shouldn't be necessary [16:28:10] I guess switches are e_object but not registered via AddSystem so their refresh isn't called? [16:30:29] okay now I'm doubting my code [16:31:41] they *should* be registered they won't draw power otherwise [16:31:52] I'll dig into it later [16:33:48] I can quickly check if the refresh function is already called [16:39:01] I am not seeing yet though how the switch itself is registered with the electrical system [16:41:20] it is though [16:41:31] if I comment out the refresh call, it still gets called [16:41:39] so it seems like it is redundant [16:41:47] just need to figure out how haha [16:52:56] or not [16:53:12] I had added a debug string to UpdateSourceState() [16:53:17] but that also gets called during loading [16:54:20] in the past we have handled these switches differently [16:55:02] we would have added a line in [16:55:06] Saturn::PanelSwitchToggled [16:55:15] instead of a refresh that gets called every timestep [16:55:41] which should be fine as long as you do the re-wiring at scenario loading [16:55:51] and then only when the switch state is changed [16:57:04] interesting [16:57:11] I get an error when loading in debug mode [16:57:19] in E_system::Create_ElectricLight [16:57:27] Run-Time Check Failure #2 - Stack around the variable 'flashing' was corrupted. [17:15:54] no idea what causes that yet [17:32:16] that doesn't sound good [17:36:57] sounds like a buffer overflow [19:34:08] it seems to be your sscanf line for the config file [19:38:12] but it only fails at the end of the function [19:38:48] maybe it doesn't like loading the bool flashing with %d [19:39:19] if I make flashing an int, let it load it with %d, and then in the ElectricLight constructor I use (flashing != 0) [19:39:23] then I don't get that error [19:44:51] ok, now I am seeing really weird things during debugging, I need to rebuild :D [19:51:30] it loads from scenario [19:51:34] first line for the switches is [19:51:35] ASCPYawSwitch 0.000000 0.000000 [19:51:59] it calls that LoadState function, but it somehow calls ThreeSourceSwitch::LoadState ??? [19:52:12] and from there it calls ThreeSourceTwoDestSwitch::UpdateSourceState ???? [19:52:24] nothing of that makes any sense [19:55:02] hmm [19:55:22] so, if a line from the scenario is loaded, it literally calls the LoadState function of every single switch [19:55:37] and in the LoadState function it decides if it even is the correct switch [19:56:04] but some LoadState functions also call UpdateSourceState [19:56:35] and that seems to be called for every single switch in the scenario [19:56:50] I don't think that does any harm, but it's very inefficient [19:57:58] n7275, and you didn't cause this haha, that was there before [20:03:49] and my original reason for checking all this, the refresh function for the rendezvous light does need to be called [20:51:30] night! [23:35:50] .tell indy91 whoops was afk the whole afternoon. I'm glad it wasn't me this time haha [13:17:32] I thought it was a good idea to make some of my little tools available that I have created over the years [13:17:41] started with this one: https://github.com/indy91/RTCC-TLI-Presettings-Card-Format [14:14:06] hello [14:14:21] that looks cool [14:20:47] I made that when I didn't want anymore that the RTCC needs to access the Saturn class directly to get LVDC parameters to simulate TLI [14:21:31] the RTCC files this creates (with TLI in the name under Config\ProjectApollo\RTCC) aren't really human readable [14:21:45] but they follow the punch card format that was used to read the data into the RTCC computers [14:53:01] ooo that document even defines what the card identification numbers should look like [14:58:13] yeah, has the full format of everything [14:58:37] MSFC sends the data via tape, it gets converted to card at MSC and that gets loaded into the RTCC [14:59:10] and in our RTCC config file it is 1 line = 1 card [15:05:13] as a proper tool this could probably use some work, maybe have you enter the three input variables via command line or so [15:05:36] this is just how I used it, with 5 minutes of looking over it today [15:06:24] I had it as a VS project, but to be more platform independent I only added this file for now, as it is the only file [15:06:29] and no sprinf_s :D [15:06:34] sprintf_s* [15:07:38] haha, I tried building on linux and rather quickly discovered those [15:09:53] should be all snprintf [15:10:01] that should be compatible, right? [15:14:09] my mistake. it is [15:14:21] it was the scanf_s [15:15:26] *sscanf_s that is [15:15:51] oh right, I overlooked that [15:15:53] I can change that [15:17:46] if there is a good function that VS doesn't complain about but also works in Linux [15:17:53] VS doesn't like sscanf anymore [15:20:19] what a pain [15:21:22] Thymo may have a better idea, but I found this https://docs.microsoft.com/en-us/cpp/c-runtime-library/secure-template-overloads?view=msvc-170&viewFallbackFrom=vs-2019 [15:22:13] All those _s functions are Windows only special sauce [15:22:16] it does suggest that I use _CRT_SECURE_NO_WARNINGS if I want to still use it [15:22:24] sscanf I mean [15:22:26] or sprintf [15:22:28] Both Windows and Linux support the POSIX variants [15:23:12] I'm not really finding a good equivalent to snprintf for sscanf [15:23:35] any suggestions? [15:25:29] I don't see any problems with snprintf. Sscanf could only be problematic if your format string is bad and the output ends up larger than the place you're storing it in [15:25:36] Is VS complaining about those too? [15:27:32] error C4996 'sscanf': This function or variable may be unsafe. Consider using sscanf_s instead. To disable deprecation, use _CRT_SECURE_NO_WARNINGS. See online help for details. [15:28:27] I can just do _CRT_SECURE_NO_WARNINGS I guess [15:29:08] Maybe we should do a #ifdef WIN32; #define _CRT_SECURE_CPP_OVERLOAD_STANDARD_NAMES; #endif [15:29:21] or #define _CRT_SECURE_CPP_OVERLOAD_SECURE_NAMES 1 [15:29:33] Then MSBuild will replace anything it is not happy with with the _s variant on Windows [15:30:39] haha we're frequency and phase locked today [15:31:46] OVERLOAD_SECURE_NAMES requires you to replace the functions with the _s variant and it will automagically insert the size. However the _s variants don't exist on *nix so OVERLOAD_STANDARD_NAMES is probably more portable. [15:35:29] or [15:35:30] #ifdef _WIN32 [15:35:31] #define _CRT_SECURE_NO_WARNINGS 1 [15:35:31] #endif [15:36:04] that actually builds for me, your two variants don't for some reason. [15:37:21] But does it solve, or hide the problem? :p [15:37:45] it hides the not-a-problem of using sscanf safely :D [15:38:53] i think _CRT_SECURE_CPP_OVERLOAD_STANDARD_NAMES doesn't work with sscanf [15:39:02] it seems to work for sprintf though [15:41:06] Maybe we can just disable it for sscanf then. [15:41:23] Anyway, need to pop off again. Having dinner at a friend's place. [16:47:05] by the looks of the forum, Jordan appears to be working on linux-orbiter [16:49:48] ah interesting, some NASSP screenshots [16:50:08] oh I saw you did a bit more with the Fortran code [16:50:45] the atmospheric density function it has uses the 1962 US standard atmosphere [16:50:49] and that's what I am using, too [16:50:51] in our RTCC [16:51:26] but I came across a document from December 1967, Apollo Missions and Navigation Systems Characteristics [16:51:47] and it suggests to use, for below 90km, a supplement to the 1962 atmosphere [16:52:16] the biggest discrepencies I found were at 80km, between the 1962 atmosphere and the realistic models that Orbiter uses [16:52:35] the IBM RTCC document does also say to use the 1962 atmosphere, but it's from May 1967 [16:52:53] so maybe I would get a bit better results if I use the modified atmosphere below 90km [16:53:17] the supplemental document has several versions, for January and July, at 15° latitude increments [16:55:19] these errors cause some differences on the Earth Entry PAD [16:55:29] the entry guidance switches to P67 at 0.2g [16:55:40] but the entry angle there is very shallow [16:55:55] so the 0.2g time is up to 20 seconds in error [16:56:06] and you would check the downrange error at that time [16:56:30] so the difference is large enough that you would almost have to declare the PGNS no go for the reentry [17:00:01] oh wow [17:00:11] that is significant [17:00:28] I also found this document http://mwhume.space/Files/TranscribeMe/todo/19680023890.pdf [17:01:12] and http://mwhume.space/Files/TranscribeMe/todo/19680023891.pdf [17:01:17] right, I think I have seen this [17:05:17] I'll need to make some comparisons [17:05:49] if the modified atmosphere model will actually be better [17:11:21] I wonder if we could add another earth atmospher model, that took historical F10.7 values rather than a static a erage [17:11:39] *average [17:13:46] oh yeah, we likely could [17:13:53] atmosphere models seem to be rather flexible [17:14:06] if they can call the Orbiter API [17:14:13] to get the MJD or so [17:14:16] and then interpolate [17:16:51] would be useful for Skylab [17:20:02] also in general, there are differences between the 1962 model and what Orbiter does by 50% at orbital altitudes, too [17:26:07] and yes [17:26:10] EarthAtmosphere_J71G [17:26:16] it calls oapiGetSimMJD [17:26:29] so we could have a database of flux numbers [17:39:33] but for now I am just happy that I manage to finish more projects than I am starting haha [18:33:36] I would like to do that at some point haha [19:03:22] I'm back [19:09:29] hey [19:16:22] I had a really nice spinach pesto pasta for dinner :D [19:29:38] oooo nice [20:13:57] indy91: I'm working on the DSKY wiring again. You mentioned that wiring the DSKY might not be a good idea last time. Why did you think that? [20:13:58] https://github.com/orbiternassp/NASSP/tree/agc [20:16:39] hmm I don't really remember. Was this about differences between CSM and LM that I was worried about maybe? [20:17:23] You were worried about introducing CSM/LM specific code into the currently agnostic DSKY [20:17:40] Convo was in 5-16 in the logs [20:18:50] ah right, it was about the LCA [20:19:21] The differences between the LM and CSM wiring is to such an extent that I need some glue somewhere. I don't think doing it in the DSKY causes too much trouble, besides maybe having to be linked against the vessels now. [20:19:54] But the DSKY is already so NASSP/Orbiter specific that I don't really see it being used for another purpose anyway. [20:20:11] Unless you want to use it for DIGFLY if we ever find itor something [20:22:12] yeah I guess you would have to add some common class in both CSM and LM that does the lighting controls [20:22:37] sounds complicated [20:23:55] I think the way I chose is minimally invasive [20:24:17] It will get some small additions when we add integral lighting for the keyboard. [20:24:37] minimally invasive sounds fine [20:26:24] looking at the Systems Handbook, there isn't really an LCA equivalent in the CSM, it's probably just a bunch of wiring and some equipment built into panel 100 [20:28:23] No instead of the LCA it has that one transformer [20:28:38] Between the DSKY and the dimmer. T4. [20:29:20] yeah [20:30:02] and some more associated with the control knobs [21:04:16] night! [11:34:30] Good morning! [11:34:46] STC, this is Apollo 9, T -53 minutes [11:36:27] morning where? :D [11:36:43] In Spain and in Florida :) [11:37:06] *In Spain (RL) and in Florida (sim) [11:37:18] ah afternoon in Spain begins after the siesta, I understand haha [11:37:25] Exactly [11:37:28] Remember [11:37:34] Spain in 2 hours late in summer [11:37:39] 1 hour late in winter [11:39:41] *is [11:40:03] So, things that will go wrong on this training: I will fail the docking, I will be unable to pressurize the LM. I will fail the extraction of the LM [11:40:14] and something else ;D [11:40:27] I'm not sure you will be able to fail then extraction haha, it's easy [11:40:48] pressurizing the LM properly takes a little bit of experience, but not difficult [11:40:54] docking takes a bunch of practice to do well [11:40:56] Last time I did it was like 12 years ago :) [11:41:17] I don´t undesrand some parts on the flightplan that say "Decal" [11:41:26] In reality that is my biggest concern [11:41:42] What is the meaning of "Decal"? [11:44:51] uhh [11:44:54] good question [11:46:12] maybe ask one of our English speaking folk [11:47:10] Habrá que recurrir a eso [11:50:02] Oh, by the way: [11:50:04] https://prnt.sc/78zv6dhhHmDe [11:50:27] Why do this text overlaps? Is this a known issue? [11:51:18] font size is weird in External MFD. Does it also overlap on the 2D panel? I have this problem constantly in the RTCC MFD, I wonder if there is something I can do [11:52:22] On 2D panel also overlaps [11:53:11] Even if I change the size of the external MFD. Font resizes accordingly... [11:53:23] Then two of the texts need to be shortened a bit [11:54:25] And... what does the text say? I think that I will need some of these controls on 9, right? [11:54:54] to the right it is just coolant loop tests [11:55:01] I don't think you ever normally would use them [11:55:05] more a debugging thing [11:55:14] on the left it just says back [11:55:16] And the hose? [11:55:29] and CRW to set the number of crew in CSM or LM [11:55:43] the hose is for better air circularization [11:55:57] we get the same issue but for different reasons, a CO2 buildup in the LM [11:56:05] the hose helps with that [11:56:20] Aha [11:56:36] they basically connected a hose to the CSM suit loop, and let it push air into the LM cabin [11:56:55] which slightly overpressurizes the LM cabin, pushes air back to the CSM, which removes the CO2 [11:56:59] when the LM is unpowered [11:57:33] I understand [11:57:58] you can kill the crew when you first activate the LM ECS and open some valves [11:58:01] too much CO2 :D [11:58:29] if you have the LM crew already in their suits [11:58:53] ^Added to the list of things that can go wrong today :D [11:58:54] I am practising up to GET 6 hours. [11:59:17] nah, won't go wrong today, no entry into the LM on the first day I think [12:02:15] By the way, what happened with 1885? [12:03:57] the release? No idea [12:04:01] was there a 1885? [12:05:20] That is why I ask, because it´s 1884, 1889, 1890, 1891,1892.. etc [12:25:40] Quick question; is the tape stopped after SECO on Apollo 9? [12:52:10] not sure [13:24:09] hey [13:24:33] "Decal" https://en.wikipedia.org/wiki/Decal [13:25:26] hey Matt [13:25:28] no idea why that particular word is used in the checklist [13:25:44] yeah, I don't get it either [13:25:53] CM/LM Pressure Equalization (Decal) [13:26:00] Tunnel Hatch Removal (Decal) [13:26:09] Docking Latch Verification (Decal) [13:26:21] as the heading for these parts of the launch operations checklist [13:26:54] maybe it means "click the texture" [13:27:10] Hey n7275 [13:27:18] Yeah, I though the same... [13:27:32] the lines I am quoting are from the actual launch checklist [13:27:34] I knew the decal word from my plastic models [13:27:37] not ours [13:27:53] so the word decal is taken from the actual checklists [13:27:57] no texture to click there :D [13:28:32] So... what to do there? Just Imagine yourself checking the things? [13:29:52] well I have no idea then lol [13:31:20] clearly there are some dialect differences between 60's Texas and 2020's Maine, American English.... [13:32:11] :D [13:33:42] or the Britsh English as taught in German schools of the 00s [13:35:09] Houston, Apollo 9 [13:35:23] 5 balls on the first P52 [13:36:52] soon you will learn that you have a docking probe on the CM and that you can extend it [13:38:38] Exactly [14:20:57] The time has come [14:38:26] https://prnt.sc/rGeclgXPUJDL [14:38:39] Go to P00, I guess... [14:39:15] That is after doing the V25N17E and V25 N22E [14:40:37] if you want to, it's not strictly necessary [14:41:17] Went to P00; 'DON HELMET AND GLOVES'. Do I do something with PAMFD? [14:42:42] nah [14:42:45] not in the CSM [14:42:52] Oukay [14:42:53] in the LM you have some options there [14:43:01] either suited or in cabin [15:41:53] https://prnt.sc/UGZC1MIYlilO [15:48:15] catch that spider [15:54:52] https://prnt.sc/-7XbCL68PdKn [15:55:01] https://prnt.sc/WyLVQVN4G-E8 [15:55:08] Houston, Docking is complete [15:55:11] :D [15:56:34] hopefully without spending half of the RCS :D [15:56:59] Yep [15:57:03] 380ish [15:57:16] lbs [15:59:36] morning! [16:01:12] hey Mike [16:01:24] what's up? [16:01:35] Hey good morning [16:01:38] I say AS-502 flight sequence program, what say you :D [16:01:46] Training apollo 9 here [16:02:24] I say, USPS may have delivered it to the wrong mailbox :/ [16:02:30] ouch [16:03:22] so, will you even get it? Or has it been properly delivered and USPS can't do anything? [16:03:49] Cago en Satán! (as we say here when something goes bad...) [16:08:30] not sure yet [16:08:47] we'll see [16:09:38] ah damn, I'll be hoping for the best [16:12:38] Jordan and gondos have been talking on the Orbiter Forum about running Orbiter and NASSP on Linux. They have been having some success after modified some code and files. [16:12:59] the least I can do is incorporate those changes, some of them are simply bugs or oversights [16:13:05] like this: https://github.com/orbiternassp/NASSP/pull/790 [16:14:45] oh sweet, that would be awesome :D [16:18:00] we should probably take the spaces out of some filenames [16:32:05] Question, my Systems Test 4D shows 0 [16:32:19] On checklist it should read 0.5-3.2 [16:32:23] Normal? [16:35:49] I always forget, is that LM power? [16:35:55] Yep [16:36:26] LM power switch is on CSM, LM power breakers are closed [16:36:35] hmm, at the very least it should be jittering a bit [16:36:44] it should be powering some heaters in the LM [16:36:53] but they might have enough heat right now [16:36:56] Yeah, I see the jutter now [16:37:01] *jitter [16:37:06] then it's fine [16:37:43] Ok [16:39:20] it means it is connected which is the important part [16:41:50] Go for LM extraction [16:42:03] Las time done in 2009 I think :D [16:45:26] Do I need to translate after SIVB/LM SEP -> On ? [16:45:29] -X [16:45:34] Just a burst? [16:48:09] 3 seconds [16:48:11] 0.4 ft/s [16:48:26] uhhh [16:48:27] no [16:48:35] :D [16:48:43] I am with the "no" [16:48:46] that's the evasive burn [16:49:05] We´ll see in around 2 minutes. Remember, kids [16:49:14] T key is Satan [16:52:05] you do get a small DV from the LM ejection though, right? [16:52:11] I think we fixed that at some point [16:52:12] 0.5 fps [16:52:13] it was 0 DV [16:52:14] Yep [16:52:29] and now it is the standard Orbiter thing of giving 0.2 m/s of separation [16:52:45] imparting the same impulse on both (in this case S-IVB and CSM+LM) [16:53:02] so I guess no additional RCS there is required [16:53:17] once you know you are clear of the S-IVB you should quickly maneuver to the evasive burn attitude [16:58:50] Yep [16:58:58] Well, alive [16:59:25] make sure to spectacte the S-IVB, because it will do a sort of TLI burn on its own :D [16:59:55] Boy, the LM is heavy [17:00:24] oh yeah, light CSM versus full CSM+LM is like night and day [17:00:30] and the Apollo 9 CSM wasn't even full [17:00:49] https://prnt.sc/c36zl7fCaYfG [17:01:53] Note: Good time for lunch, sandwitch, as in Apollo 8´s lunar day [17:02:14] Because it was tough to fit the lunch time based on the flightplan only [17:06:11] the flight plan has an eat period "as possible" from 4:50 to 5:50 [17:06:35] but there is a lot to do, that won't be possible for all three crewmembers aka you :D [17:06:42] :D [17:06:57] And also a little bit late based on RL [17:07:03] (real life) [17:07:19] right, but you will have to adjust to their rest periods [17:07:25] But this time... Food will be prepared by me! [17:07:40] Wich can be really dangerous [17:07:42] starting with 9 they do all sleep at the same time so that is the best time for you [17:07:56] Yeah [17:08:09] Some days lunch is at 10 AM [17:08:14] unfornutately [17:08:20] But pretty regular... [17:11:33] I already forgot, when you are always launching relative to the actual time? [17:11:45] are youÜ [17:11:48] are you* [17:12:22] I've had lunch at 10:30, just get up at 5:15 and you will be hungry again by then :D [17:14:43] Lost track of you, Indy [17:14:52] Ah.. [17:15:14] When I lunch relative to the actual flightplan... [17:15:31] you said lunch at 10 AM, which means you already know at what time of the day you are launching [17:15:32] Lost you on the "always" :D [17:15:48] yeah "always" meaning "you have a system for this which I forgot how it works" :D [17:16:12] Well, I said 10 because I already processed the flightplan :D [17:16:33] Did it one or two days after 8´s slpashdown [17:16:35] Apollo 9 launched at 4pm GMT [17:16:43] That is 11 EST [17:16:47] and 11 for me ;D [17:16:51] so you are launching 11 your time [17:16:54] got it [17:17:06] Yeah, that is my "system" [17:18:51] for the lunar missions it was a bit tricker because they needed to land at a fixed time [17:19:15] I guess usually they had a really long first day of the mission, very exhausting, and that was most of the biological clock adjustmnet already [17:20:02] Aha [17:21:19] in some cases you might have a really weird sleep cycle by the end of the mission, very different from the start [17:21:40] not sure how much that applied to Apollo 9 [17:22:14] On 9 the sleep times moved around a bit... [17:22:33] I see [17:22:38] But well, in case of weird sleep cycles, it can be trained [17:22:40] yeah it won't be nicer on the following missions I guess [17:22:49] as I did with the 26 hours of activity [17:23:13] Will have to look at that... [17:23:28] But a way can propably be figured out... [17:24:54] it should be quite gradual, just after your missions your sleep cycle is wrecked :D [17:27:29] Maybe we should implement the time on the van, to recover the sleep cycle :D :D [17:28:41] S-IVB is ullaging [17:28:56] having to quarantine is a valid excuse to your boss these days [17:29:18] Not anymore in Spain :D [17:29:25] Covid? What is that? [17:30:19] some Mexican beer [17:30:31] Must be... [17:31:02] https://prnt.sc/HGgSNNAVud1n [17:34:04] Confusion again, Houston [17:34:06] "Copy SPS-1 Maneuver PAD, VERB 66, Target load [17:34:13] What is the Verb 66 refering to? [17:36:27] hmm [17:36:30] I'm not sure [17:36:52] I would have thought it uplinks a V66, but is there even a SV uplink? [17:37:06] Here yes [17:37:12] It´s doing it now... [17:37:21] Maybe it uplinks the V66 [17:37:36] How can I check it? Vector compare display? [17:38:16] I think there is only a target load [17:39:02] it must be a copy and paste error from the other SPS maneuvers [17:39:11] Copy SPS-2 Maneuver PAD, state vector update, verb 66, target load [17:39:19] Copy SPS-3 Maneuver PAD, state vector update, verb 66, target load [17:39:22] and so on [17:39:47] Ryan must have removed the "state vector update" but forgot that there is also no "verb 66" [17:40:33] so just ignore that [17:40:36] it should read [17:40:41] Copy SPS-1 Maneuver PAD, Target load [17:41:05] Ony "target load" on the MCC message [17:41:12] yeah, and that's all there is [17:41:31] the CSM+LM did a bunch of small maneuvers just now, no way they already had an updated SV from ground tracking [17:41:39] Aha [17:41:58] so just a small checklist error, nothing else [18:10:49] Houston, we have a problem [18:10:57] My view is moving itself on the VC [18:11:35] When changing  the spacecraft attitude [18:11:51] https://github.com/orbiternassp/NASSP/issues/767 [18:12:21] You are quick! [18:12:22] :D [18:13:22] I haven't really seen this myself yet, so I couldn't start debugging it [18:14:47] what do you do, roll pitch yaw rate? [18:15:02] It was roll and yaw [18:15:07] 0.7º/S [18:15:09] moreless [18:15:11] Onesec [18:15:14] Busy [18:16:24] ok I think I see it now when I do a 1°/s pitch rate at 10x [18:16:36] Struggling with the P52 attitude check... the one with Option 3 after the preferred [18:16:51] Will clarify later, as the clock is ticking [18:28:47] I think it is caused by the code that handles the shaking during engine firing [18:28:50] but not 100% yet [18:30:51] OK, back on track; I think [18:31:23] Could not do the P52 alignment check as I was always getting the "Cant move telescope to that star, out of my sight" alarm [18:31:34] Not the 405, another (didn´t check) [18:31:59] when I was selecting stars that in theory should be visible to the telescope [18:32:14] But that was a pilot error, because the procedure was kinda new... [18:32:23] 10 minutes to SPS-1 [18:33:13] I hope you actually have a good alignment [18:33:29] That is why i said "I think" :D [18:34:59] and you are just going to trust that it works without verifying? :D [18:35:10] I have Faith [18:35:26] By the way, residuals rule? [18:35:49] I have Faith, and it´s a training :D [18:36:27] But I think I am OK; it´s just a heads up posigrade burn, right? [18:40:53] not sure about residuals, I think they didn't trim them, only for the rendezvous maneuvers and deorbit [18:41:09] yeah, prograde [18:41:29] Yeah [18:41:44] As i see "Report residuals and DV counter" [18:43:12] "No not trim" the checklist says :) [18:46:31] OK, that is training complete. [18:46:51] Any hint on how to find S-IVB to look at it for its second restart? [18:48:09] it's not doing a second restart, that's not implemented [18:48:27] Oh [18:48:40] I could do it, it's just a bit annoying, lots of Apollo 9 specific code that the LVDC suddenly will need [18:48:58] Andthe LOX dump? [18:49:19] I forgot when there was a LOX dump :D [18:49:24] is that after the second restart? [18:50:14] ah after [18:50:15] 6:42:10 GET (LOX and LH2 dumps completed) [18:51:37] Well, sirs [18:51:37] Going to dinner and bed. See you tomorrow for a 4 hours training, 6 to 10 GET. I did today 10 hours because I had forgotten that I thought about doing the prelaunch yestarday [18:51:59] Thanks for the help, been a smooth train, expected to fail today :D [18:52:07] it does a LOX dump, but I might have just copied and paste the sequence of events of a later mission [18:52:25] cya! [18:52:32] Good night [18:57:23] maybe I could just let the LVDC logic cycle back from time base 7 to time base 5 at the right time [18:57:44] to simulate the second restart [18:57:48] might have to look into that :D [20:56:51] night! [21:28:50] hi guys, I think I got a small bug for you ;) [21:29:14] the forum is down so I'll tell you here^^ [21:29:20] in bool ApolloRTCCMFD::set_RTESolution(char *str) [21:29:34] there is a strange "else if (str[0] == 'RTEM')" [21:29:43] I suppose it should be a strcmp [21:55:22] .tell gondos, we'll look into it [22:00:26] I had a double login, did you get the details? [22:01:19] again in case you didn't see it: [22:01:25] in bool ApolloRTCCMFD::set_RTESolution(char *str) [22:01:30] there is a strange "else if (str[0] == 'RTEM')" [22:01:38] I suppose it should be a strcmp [22:07:49] I saw. thank you [22:10:39] ok:) [03:20:16] .tell indy91 gondos found a potential issue in bool ApolloRTCCMFD::set_RTESolution(char *str). check the logs for details [12:57:28] hi gondos [13:07:51] hi [13:26:32] indy91 is usually on soon. he's the one to ask about RTCC stuff [14:53:23] hey [14:56:13] hey [14:57:24] yeah that's probably another small bug [15:17:31] Heyy [15:17:39] How is it going? [15:41:57] hey [15:42:23] I am thinking if there maybe is a somewhat simple way to let the Apollo 9 S-IVB do the second restart [15:46:03] Nice [15:46:14] Did they get a PAD to look at it? [15:46:22] Maybe through optics? [15:48:22] I don't think there is a chance that they could have seen it [15:48:45] Yeah... [15:48:50] Very different orbit [15:49:29] S-IVB was probably so far behind that it was hidden by the Earth [15:49:41] But.. [15:49:48] Maybe stupid question [15:49:48] so not only distance too large to Apollo 9 but also not possible to be seen [15:50:24] Why does that event appear on the flightplan or on checklist MFD, if the crew could not monitor it? [15:50:40] And is a "Ground guys task"? [15:52:05] *Why does that event appear on the flightplan or on checklist MFD, if the crew could not monitor it and is a "Ground guys task"? [15:52:06] yeah not sure [15:52:29] There were some alternate sequences in the LVDC for the case the first restart can't be done [15:52:51] Any hint about the viewport movement bug? [15:52:53] I need to check but the second restart might happen at a similar time [15:53:10] and if the first restart didn't happen, they might be able to see the second one [15:53:27] Yep [15:53:28] I am fairly sure that is caused by the code that does the shaking effects [15:53:34] during launch [15:53:37] need to investigate more [15:53:38] Aha [15:54:09] How does it behave for you. If I do 1°/s pitch rate then the view shifts upwards but at some point it actually goes down again [15:54:38] Almost seems to depend more on the attitude than the attitude rate, although that would be really weird [15:54:39] Will check that in a few minutes [15:55:05] As I will have the Daylight star check, and I assume that an attitude change is required [15:55:14] BTW, if you need help to debug the stuttering I offer myself as volunteer for that [15:55:48] Thymosaid about using a Profiler, I don´t know how that works but well, if I can help... [15:56:32] did you ever notice the viewpoint bug with the CSM alone? [15:56:42] ^nope [15:56:46] Not on 7 [15:56:49] Not on 8 [15:57:03] On trainings or on RTS [15:57:08] if not, I suspect the way that vibration code calculates the acceleration might not work right for docked vehicles [15:57:38] FYI; I will continue to write the Apollo 8 debrief on the weekends [15:58:20] To debrief each FD takes some hours from my soul :D [15:58:29] haha [15:58:32] I am reading it [15:58:42] And I don´t know if I will have soul remaining to debrief FD4 (lunar daay) :D [16:01:23] the calculation our accelerometers use are a lot more complicated than you might think would be necessary [16:01:53] but there is a reason for it, Orbiter API functions not really returning the right numbers for it [16:02:07] and this vibration code does not use the same calculation as our accelerometers [16:02:18] one comment from our IMU code [16:02:27] "The force vector matches the global velocity change of the last timestep exactly, but isn't used because GetForceVector isn't working while docked" [16:02:42] now that sounds suspicious [16:04:26] Aha [16:04:32] Very suspicious... [16:04:39] Houston, I paused; [16:04:41] https://prnt.sc/0uPDuEkUEMMe [16:05:05] Ok, what scared me was "To be performed following P52" [16:05:19] What P52? Any previous P52? [16:06:42] I'm not seeing a P52 [16:07:34] That is the thing :D [16:08:11] But I did one not so long ago... Maybe at the hour 5? I am at 6:50 GET [16:08:12] the DTO mentions that there should be a P52 before the test [16:08:15] but question is how long [16:08:57] the P52s done on the first day were at [16:09:01] 0:39, 5:18, 8:24 [16:09:02] that's it [16:09:09] 5:18 then... [16:09:10] Will try it this way, "without". I will maneuver to the PAD attitude, and follow the instructions... [16:09:48] add it to the list of small checklist issues to tell Ryan [16:10:03] But runrise was some seconds ago. This triggers at 6:50:00. Maybe should trigger at 6:40:00 ? [16:11:29] when did you have sunrise? [16:11:47] 6:49:45 [16:12:31] wow, then the flight plan is really not very good for the actual launch time [16:12:40] .... [16:12:44] Something is wrong here [16:12:50] Let me check [16:12:55] flight plan has sunrise at 07:05 [16:13:07] hmm [16:13:12] but it is 1600 GMT launch [16:14:18] uhh [16:14:25] https://prnt.sc/XIMswBVNpM13 [16:14:29] PAD is wrong [16:14:30] would you believe that the crew had almost the same conversation as we just had? [16:14:40] Yes, I believe :D [16:14:45] PAD is hardcoded actually haha [16:14:57] Because I just had sunSET [16:15:31] So; what do I do, Fail everything on this test? [16:15:47] 006:35:54 McDivitt (onboard): It says, "GET start, sunrise - Oh, sunrise minus 15." [16:16:35] that time is SR minus 15 minutes [16:16:45] but the PAD doesn't really say that [16:17:25] "TIME OF SUNRISE AT START [16:17:27] OF qAYLIGHT STAR CHECK" [16:17:28] https://history.nasa.gov/afj/ap09fj/006_day01_rev005.html [16:17:32] read from 6:35 [16:17:39] they had this same confusion [16:18:26] and the AFJ has this description of the PAD [16:18:28] Sunrise time - 15: GET 006:49:45.00. The time of the start of the daylight star check. The flight plan PAD describes this field as the time of sunrise at start of daylight star check. However, this figure is the start of the daylight star check procedure which is (sunrise - 15 minutes) and the crew interpret it correctly. Sunrise is thus predicted to occur at 007:04:45.00. [16:18:49] So not sure what to do haha [16:21:24] Well; Not fail :D [16:21:35] Waiting for 04:45... [16:21:40] And I should get 19... [16:21:46] (star 19) [16:27:44] Well;Sunrise, for me the dimmest is star 24 [16:34:55] Sunrise +5, still 24 [16:34:56] 007:09:58 Schweickart (onboard): What kind of a star check is that? [16:34:57] Sunrise +10, still 24 [16:35:15] Conclusion: Orbiter´s astronaut is not blinded by light, he is a superhero [16:44:42] OK, indy91 I will give you a 1º/s yaw to the left [16:45:02] have fun with gimbal lock then [16:45:05] And see if i bounce on window 5 [16:45:30] I am yawing becase if I pitch yeah, I will have Gimbal... wait [16:45:37] You are right :D [16:45:50] It´s yaw but pitch [16:48:09] Ah... Viewport moves very slowly... [16:48:14] Tried various axix [16:48:21] Moves slowly... [16:48:37] that acceleration thing I talked about, it's quite weird [16:48:58] I did see an acceleration when there wasn't any, but only if there were attitude rates in multiple axes [16:49:06] Hey [16:49:13] Got an MN B Undervorlt [16:49:44] morning! [16:49:56] Hey! [16:50:12] How is the package delivery process? [16:50:39] indy91 Can I interrupt the batt B charge and troubleshoot this MN B Undervolt? [16:50:44] still in limbo. going to give it a few more days before I really push it, to see if it shows up [16:50:54] (is it safe?) [16:51:11] thewonderidiot Well... [16:51:21] Hope that it ggoes well... [16:51:22] TurryBoeing, sure [16:51:38] did you forget to switch off gimbal motors [16:52:15] uhhh.... Why would I need that? [16:53:31] to conserve power :P [16:54:05] There isn't really much you can do to cause bus undervolts [16:54:25] mmm... MNB is fluctuating... on 27 ish volts [16:54:29] so getting one is quite weird [16:54:50] I have all the jets on MNB. Don´t know why but it is based on checklist [16:54:58] and it surprised me... [16:55:09] Will put some of those on MNA [16:55:15] So you only get an undervolt when you fire the thrusters? [16:55:31] Negative; MNB undervolt still on [16:55:52] then the Auto RCS switches won't do anything [16:56:02] I don't think it can be the LM [16:56:09] the CBs for LM power would pop before that [16:56:18] you must have something on that is not normally on [16:56:21] I thought about the LM [16:56:29] you can check if you want [16:56:41] Want scenario? [16:56:43] the LM can draw 10 Amps at most I think [16:56:50] sure I can check [16:56:58] but I am sure you have something on that should be off :P [16:57:23] DS [16:57:50] got it [17:00:45] There was a document with troubleshooting instructions for various lights [17:01:02] Do you remember what was it and where it was ? [17:02:52] AOH Volume 2 [17:02:58] your FC3 is working hard [17:03:24] but I am not seeing an obvious issue yet [17:04:34] uh oh [17:05:00] what did you do, Matt [17:05:02] :P [17:06:32] haha [17:06:49] I still think it's some wrong CB state or so [17:07:04] Ok, got a thing to do -> MN B RSET - RSET [17:07:18] Boom shakalaka [17:07:22] Light off [17:08:06] Still 27 ish volts, but not flickering now... FC3... Flow flickering... [17:08:10] But well [17:08:51] Batt charge resumed; suspecting about spot light. Still on and wondering if it should be off [17:09:48] probably should be off [17:10:10] we have the launch etc. checklist which switches it on, but then not the right checklist for later to switch it off maybe [17:10:28] and the reset doesn't really fix anything haha [17:10:33] it just makes the light go away [17:10:47] Turned off... FC3 still flickering [17:11:18] n7275, FC3 outputs 39A [17:11:28] and that makes the voltagr about 27V [17:11:49] I guess it must have dipped below 26.25V for a moment, that caused the undervolt light [17:11:53] Well, flow on AOH says... "TRANSIENT UNDERVOLTAGE OR OVERLOAD" [17:12:14] AOH agrees with you, indy91 [17:13:11] ah wait a minute [17:13:25] the normal fuel cell config is [17:13:32] FC1 and FC2 on MNA [17:13:37] FC2 and FC3 on MNB [17:13:42] you only have FC3 on MNB [17:13:45] 2 and 3? [17:13:54] uuuhhhh..... [17:14:13] -looking for excuse- [17:14:45] could also be the checklist being wrong or something [17:15:52] nope [17:15:55] can't blame the checklist [17:15:59] MainBusBSwitch2 [17:16:14] maybe a temperature thing [17:16:17] it has that switch to off in the backup crew prelaunch checklist and deorbit checklist [17:16:34] and switched on in the prime crew prelaunch checklist [17:16:37] and nothing else [17:16:52] n7275, hmm? Does it automatically disconnect based on temp? [17:17:58] Word Prelaunch checklist. "Chapter 2"  (Final verification & systems checks) Gimbal Drive & Trim Check [17:17:59] FC MNA 1 & 2 - ON [17:18:00] F*M* MNA 3 - OFF [17:18:01] FC MNB 3 - ON [17:18:02] FC MNB 1 & 2 - OFF [17:18:19] Valid excuse? Should I stop using word checklists? ;( [17:18:34] oh are you actually using those age old documents? :D [17:18:54] Invalid excuse detected [17:19:28] Well, yes I am; did that on 7 and 8. I think they are more confortable for me [17:19:38] hmm [17:19:42] as I prefer to read long things on paper [17:19:53] I am seeing some procedures that have FC3 MNB in off [17:20:01] But we can probably look for a solution [17:20:08] uhh [17:20:16] FC2 MNB I mean [17:21:17] yeah the AOH Volume 2 has that off [17:21:28] it shouldn't disconnect for anything other than over-current [17:21:56] or reverse current [17:22:19] Well, the switch is in off, I didn´t turn it on [17:22:36] The switch is sprint loaded, n7275 ? It can pop off? [17:22:41] *spring [17:22:52] ? [17:23:09] no I don't think so [17:23:33] the NASSP standard procedure seems to be FC2 MNB to on, but the AOH has it in off [17:23:38] I mean, in case of overcurrent or something, the switch can turn itself to off? That is what I mean with spring loaded [17:23:59] no, it's springloaded to center [17:24:04] if you switch it up [17:24:13] Correct... [17:24:14] the switch can stay in the center or down position [17:24:16] but not up [17:24:38] do we have too much stuff on MNB? [17:24:48] or maybe the power sharing doesn't work right [17:25:00] Well, we had all the jets on MNB before [17:25:14] that probably caused the under voltage [17:25:17] some jets firing [17:25:18] and I was playing with the jets before the alarm [17:25:20] all drawing froM NB [17:25:22] MNB* [17:25:33] and then it was above the threshold again if you don't fire [17:25:53] I though it was some sec fuel press for some quads and ignored the alarm for some seconds [17:26:03] and then I looked at the CW panel... [17:26:09] and saw that [17:27:11] So, am I in the correct FC config? It´s time to ditch my beloved word checklists? [17:28:17] the word checklist has the same as the AOH [17:28:43] but in NASSP, for some reason, we usually have FC2 on MNB to even it out [17:28:57] the issue could be in multiple places [17:29:09] is 39A draw too high for MNB? [17:29:20] does the voltage drop too much with 39A? [17:29:45] but I guess what you should do for now, have FC2 on MNB [17:30:48] and I can just turn it on, right? [17:30:54] as is a FC... [17:32:31] all the fuel cells are on all the time [17:32:40] you are just switching FC2 onto Main Bus B [17:32:54] those switches just decide where the power goes [17:32:56] "Tieing" [17:33:20] Maybe misspell... "Tie ing" [17:33:30] I think you get me :D [17:33:43] that sounds more like before a wedding [17:34:16] Well, FC 2 on MNB also [17:34:21] FC2 on MNA and MNB [17:34:28] yes [17:35:03] Amps still high (obviously) [17:35:13] But more juice [17:35:30] Gonna put the jets all on MNB as before... [17:35:35] yeah I think the Amps are somewhat normal [17:35:41] at least compared to other scenarios [17:35:51] nah, I don't think that is a good idea [17:35:56] I don't know why they did that [17:36:20] or maybe they didn't even do it, it's based on a checklist that wasn't flown I believe [17:36:25] Well, let´s see what happens... They are on MNB; soon a proper sleep period [17:36:50] if you loose MNB with all thrusters on MNB you will loose all thrusters [17:37:04] Still have CM :D [17:37:20] and LM [17:38:02] I think you need to treat the checklist a bit less like god given haha [17:38:15] I do that mistake... [17:38:22] suddenly there is an error or small omission, mostly due to NASSP [17:38:29] and then you are drifting off the entry attitude [17:38:38] :D [17:39:20] and the real checklists or PADs aren't perfect either [17:39:35] like that one PAD that says sunrise but the time on it is actually 15 minutes earlier... [17:39:49] Well, that had Houston... [17:39:59] Pn to P52 [17:40:02] *On [17:40:44] There is something that concerns me... I am getting some rates. [17:40:48] on attitude [17:41:01] When on SCS or CMC FREE [17:41:42] torque due to drag maybe [17:41:48] LM is big [17:41:57] Or new aerodynamics? [17:42:02] could be yeah [17:42:11] wasn't implemented yet when you flew 7 [17:42:13] I think [17:42:22] yeah [17:42:33] although with the LM attached the effect should be smaller [17:42:36] but it was still there [17:42:42] Well [17:42:48] More thing in the air [17:43:05] Better said... More unaerodynamical thing on the air [17:43:06] and your perigee is 100 NM at the moment, right? [17:43:09] that's somewhat low [17:43:12] Yeah [17:43:21] Apollo 7 went down to 80 NM perigee [17:43:34] and the effect was so strong that they used 90 NM minimum on Apollo 9 [17:45:02] oh actually with the LM the effect can be bigger, but the LM doesn't have proper aerodynamics like the CSM [17:45:14] "The reported tendency of the spacecraft to seek an in-plane attitude is to be expected in earth orbit. The approximate predicted torque from aerodynamic drag for the docked spacecraft is 2 ft-lb at 100 miles altitude with the X-axis oriented out-of-plane. The corresponding torque on the command and service module under similar circumstances would be 0.5 ft-lb." [17:45:15] Yeah, that is my theory [17:46:21] the worst attitude is 90° relative to the velocity vector [17:46:34] so CSM point up/down or left/right (out of plane) [17:47:04] Apollo 7: https://i.imgur.com/X07TgAH.png [17:47:16] at 90 NM perigee after SPS-3 [17:50:04] Yeah [17:50:10] Taking about Apollo 7 [17:50:26] GOOD GOOD WX [17:50:27] GOOD [17:50:27] WX [17:50:35] Does it give you memories? :D [17:50:45] nice formatting [17:50:50] but the weather is always good [17:51:02] the Block Data calculation just likes it that way [17:51:11] I had dreams about METAR and weather in Orbiter [17:51:21] Maybe with Skybolt... [17:51:26] Some day... [17:52:19] then Apollo 11 needs to do the mini skip reentry [17:52:23] for weather avoidance [17:52:37] Oh [17:52:38] Donñt know about that one [17:53:24] Apollo 11 was the only mission that got P65 during reentry [17:53:30] they extended the reentry range [17:54:48] Aha [17:55:48] but still not a proper skipout [17:56:20] And what was the bad weather? Storm? Typhoon? [17:57:07] something like that [17:57:13] for reference: [17:57:19] Apollo 8 - 1350 NM [17:57:53] Apollo 11 - 1285 NM (planned) [17:57:56] 1400 NM actual [17:58:13] Apollo 8 reentry range is very close to getting into P65, but not quite [17:58:18] and Apollo 11 was just above the edge [17:59:00] for me Apollo 8 reentry always feels weird because there is a very low G phase [17:59:12] none of the later missions had that (at least not planned) [17:59:25] Yeah [17:59:48] But the low G force was used by me as time to relax [18:00:14] Maybe also by tjem :) [18:01:06] haha [18:01:12] for the whole 30 seconds it lasts [18:01:24] there is a whole article about this Apollo 11 weather [18:01:25] https://history.nasa.gov/afj/ap11fj/recovery-weather.html [18:01:27] Enough time [18:02:09] Gonna manage this attitude after the FC purge... [18:02:15] I am too sideways [18:02:47] And obviously getting a yaw rate [18:07:28] usually it will push you in-plane, but if you are at 90° angle of attack it could even try to get to 0° angle of attack through gimbal lock [18:07:42] so you have to be a little bit more careful than before. But not much. [18:07:58] I haven't tested it a lot and you have to be qutie unfortunate for this to cause gimbal lock [18:08:02] I have tested* [18:08:15] Yeah [18:15:15] Time to power down everything [18:15:25] More memories from 7 [18:15:30] Even P06! [18:22:06] and then you can let the aerodynamics do what they want [18:23:35] Yup [18:24:16] When is LM activation? [18:24:30] Or an inspection is done before touching any switch? [18:26:42] you don't enter the LM until day 3 [18:28:41] 42 GET [18:28:45] And some minutes [18:42:48] Well guys; Dinner time, sleep time [18:42:53] See you! [18:45:11] https://i.imgur.com/RKjrx6z.png [18:45:25] I finished drawing CDU Tray S last night, except for the pins [18:45:53] so I'm getting very close to done with the backplane viewer, at which point it will be time to fully disassemble the CDU and map out all of the unknowns / ambiguities :) [18:46:58] fully disassemble sounds scary :D [18:47:23] really I can't go too much further than I already have [18:47:47] it's just, pulling all of the modules out at once, instead of only one or two at a time [18:47:58] ah, that makes sense [18:55:20] so it will look a bit like the AGC did here https://i.imgur.com/2amAv7O.png [18:55:51] ha, what a view [18:56:39] not guiding much in that state [18:56:53] definitely not haha [18:58:29] I'm curious if I'm going to find any more surprises on the modules, like I did with the Mode module [18:58:39] I definitely haven't seen both sides of every module yet [18:59:57] maybe some more spacecraft reassignment surgery? [19:01:16] can't tell that with the modules, until I find component serial number tracking info.... which I'm pretty sure only AC maintained, internally [19:01:29] but there might be other part replacement surgeries where they dug in through the potting [19:03:10] and I need to check but I'm like 90% sure some of the modules in my Tray S are much too new to have been the ones installed in it when it was part of the Apollo 7 CDU [19:04:05] I am very curious if my mapping of the Tray S backplane is going to turn up the problem that caused the "not fit for flight" marking [19:04:25] like if it's a bad wire on the backplane, or if it's just some mechanical issue [19:05:12] unlike the AGC where I only checked unknowns, I'm currently planning on doing this one all the way -- beeping every single connection [19:05:21] oh boy [19:05:37] since my time with it is not as limited, and since its backplane is far far far far less complex than the AGC [19:05:44] but yeah, could be something simple that prohibited it from flying, something that doesn't have to do with actually running it [19:08:28] yep [19:08:48] something else interesting about the CDU that I realized [19:09:10] I'm pretty sure that unlike the AGC, there is no reason why I can't run Tray X all by itself, without Tray S even attached [19:09:34] functionally what do those two trays do each? [19:09:45] Tray S is just the three IMU channels [19:09:56] Tray X is all of the central logic and the RR/optics channels [19:09:57] read and error counter? [19:10:31] for each channel: Digital/Analog Converter, Error Counter, Coarse System, Read Counter, Main Summing Amp, and Quadrant Select [19:10:44] right [19:11:24] but the absence of the IMU channel modules won't have any impact on the functioning of the central logic or the RR channels [19:12:23] yeah, I guess a separate checkout of the Tray X input/outputs could work and already tell you a lot [20:55:09] night! [15:02:00] hey [15:36:33] hey [15:39:23] i think I am happy with my DKI update, so it can be tested now [15:49:08] Hey [15:49:16] hello [15:50:13] ready for a lot of SPS burns? [15:54:27] zzzzzzz [15:54:47] ah right, T button is the devil, so you are going to be bored for a while [15:55:19] zzzzz :D zzzz [15:59:29] indy91 Saw on tthe flighplan a burn with MTVC for the last 45 seconds of burn [15:59:40] Is that equivalent to SPS-5 on 7? [15:59:48] yes [15:59:54] :C [16:00:02] Well, it´s training time [16:00:07] Can practise it [16:00:15] And we can use the asterisk [16:02:35] it's not a manual shutdown at least [16:02:40] was Apollo 7 SPS-5 manual? [16:03:10] looks like it [16:03:56] so you can fully concentrate on flying to the error needles [16:08:23] Yeah [16:08:49] Remember that I couldn´t shutdown the engine and orbit went a but to hell [16:09:11] you only did slightly worse than the actual mission I think :D [16:12:56] Oh [16:13:07] Didnñt know that :) [16:17:53] they overburned by 50 ft/s [16:18:10] I just vaguely remember that you did something similar [16:22:28] 100 ft/s, me [16:22:37] ouch haha [16:22:50] But the burn was designed for that not to be a big problem [16:22:57] and it didn't turn out to be one [16:23:58] Well, I was ahead of schedule and MCC didn´t like that [16:24:39] Ahead of schedule or behind? Dont remember. Maybe I posted that on the debrief [16:24:51] yeah I need to read the debrief again [16:25:33] Offtopic [16:25:36] https://www.marinetraffic.com/en/ais/details/ships/shipid:991737/mmsi:311000274/imo:9656101/vessel:ANTHEM_OF_THE_SEAS [16:25:47] Today at the port of my town [16:25:54] What a beasty ship... [16:26:43] yeah, those cruise ships are giants [16:27:07] biggest one I was ever on was a cruise ferry to Norway, that also seemed very large [16:27:26] I was never on one; only on small ships [16:27:45] The ship I was on is only 2/3 of the length of the Anthem of the Seas [16:28:51] hard to imagine :D [16:29:18] Yeah [16:29:36] 3 saturn fives together [16:29:41] In horizontal position [16:32:32] looked at the debriefing, I think everything was expected considering the overburn [16:32:43] schedule was a bit messed up, but not much you can do there [16:34:23] Yup [16:34:35] So the 3 burns of "tomorrow" should be fine [16:37:34] "The residuals on shutdown were [16:37:35] plus 2.7, minus 2.1, and minus 2.6. " [16:37:43] that's what you are up against with SPS-3 :D [16:40:55] I forgot, are you using joystick or numpad? [16:46:00] Numpad [16:47:29] For joystick I think that I need vesim or something like that right? [16:47:35] And a joystick :D [16:47:55] Vesim just has some additional features, it's not required [16:47:57] Got the thustmaster hotas, but it´s old... [16:48:34] And maybe I need two josticks [16:48:47] (THC and RHC) :D [16:49:07] nah, there are no joysticks that accurately depict a THC or TTCA [16:49:15] Correct [16:49:29] a good joystick for ACA/RHC and numpad for TTCA/THC is the best setup imo [16:50:16] Maybe joy on the right hand and a USB numpad on the left hand [16:50:40] Joy can always try to do a THC with an arduino, but maibe too much PITA [16:51:06] MTVC with numpad works just as good [16:51:11] just different technique [16:51:14] more of a tapping [16:51:16] Yeah [16:56:19] are you familiar with the stroking test done with SPS-2 and 3? [17:09:17] Ah [17:09:26] Forgot that, was going to ask you also [17:09:35] Is that... Throttling? [17:09:47] But to answer; Not familiar [17:10:04] haha, no, the SPS can't throttle [17:11:02] it's gimballing [17:11:19] to cause some propellant sloshing on purpose [17:11:22] just a little bit [17:11:37] and in NASSP you barely notice it [17:11:52] it's for testing the dynamic behavior of the CSM+Lm stack [17:12:12] Gimballing? [17:12:14] SPS-2 uses 40% of the maximum amplitude of the test [17:12:18] and SPS-3 uses 100% [17:12:24] yeah, SPS TVC [17:12:29] Like a Flight control test? [17:12:44] I mean, move the TVC circling around... [17:12:59] back and forth at fairly high frequency [17:13:18] during the burns [17:13:26] basically a command added to the normal TVC commands [17:14:25] https://i.imgur.com/HRXG1KQ.png [17:14:26] Interesting [17:16:00] you start it with Verb 68 [17:18:37] It´s new on the Apollo 9 software, I assume [17:19:01] it's on the Apollo 8 through 11 software, only used on 9 [17:19:28] did they remove it from Comanche 67? [17:19:45] I think so, maybe one mission later [17:20:45] I ask because I don´t find it on the A8 CMP checklist document [17:21:19] early AGC software had a tendency to have programs for later missions included, apparently [17:21:41] the Apollo 9 LM software includes all of the lunar landing code, in a very early and very buggy state, but you can still start it up [17:21:48] but you will never ever find it in any documentation ;) [17:21:52] Apollo 8 and 9 CMC software is nearly identical [17:22:09] and originally Apollo 8 would have had a LM [17:22:19] this test was always for CSM+LM docked [17:23:13] Aha [17:23:41] stroke test got deleted after Apollo 13 actually [17:24:42] GSOP says it was deleted for Colossus 2E which was Apollo 14 [18:11:31] https://prnt.sc/GaaQyDz3pR_N [18:11:42] Always love this part of Earth [18:20:55] what is it? Himalaya? [18:21:39] I think so [19:42:46] Good night guys! [19:48:59] cya