Guidance and Control System
The Guidance and Control System consisted of a number of sub-systems for in-flight navigation and guidance. This article gives a high-level overview of the sub-systems: detailed information use will be on individual pages for those systems.
Stabilisation and Control System (SCS)
ORDEAL
Entry Monitoring System
|{{#if:|, | and }}[[{{{2}}}|{{{2}}}]]}}{{#if:
|{{#if:|, |, and }}[[{{{3}}}|{{{3}}}]]}}{{#if:
|{{#if:|, |, and }}[[{{{4}}}|{{{4}}}]]}}{{#if:
|, and [[{{{5}}}|{{{5}}}]]}}{{#if: | (too many parameters in {{mainarticle}})}}
The Entry Monitoring System is used by the crew to monitor the entry trajectory flown by the PGNCS and allows the pilot to fly a manual re-entry if required.
The main EMS panel includes a velocity/load-factor display, range-to-go display, 0.05g indicator and roll/attitude indicator.
External Links
- Apollo experience report: Command and service module reaction control systems
- Apollo experience report: Guidance and control systems
- Apollo experience report: Guidance and control systems - Digital autopilot design development
- Apollo experience report: Lunar module landing radar and rendezvous radar
- Apollo experience report: Lunar module reaction control system
