RTCC MFD
Introduction
The RTCC MFD is one of the three MFDs within the NASSP releases. Originally created to calculate the Apollo 7 rendezvous maneuvers, the MFD has expanded to include many more features which during the Apollo program were provided by Mission Control (MCC) and the Real-Time Computer Complex (RTCC).
Currently the features of the MFD are:
- Calculating rendezvous maneuvers by solving Lambert's Problem (Useable for the Apollo 7 phasing, NCC1 and TPI maneuvers).
- Coelliptic maneuvers (Usable for the Apollo 7 NSR burn).
- Generic orbit adjustment maneuvers (Usable for the Apollo 7 SPS burns).
- Return to Earth trajectories from anywhere in the Earth-Moon-System.
- All types of IMU transformation matrizes (REFSMMAT) used for the Apollo spacecraft.
- Lunar orbit insertion maneuvers, including Translunar Injection (TLI) and Midcourse Corrections (MCC).
- CSM and LM State Vector Update.
- Uplink to the AGC for Contiguous Block Updates.
- Displaying various Pre-Advisory Data (PAD).