RTCC MFD

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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).
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