The Level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and flight control functions to be incorporated into the Mission Control Center entry profile planning processor are defined. This processor will be used for preentry evaluation of the entry through landing maneuvers, and will include a simplified three degree-of-freedom model of the body rotational dynamics that is necessary to account for the effects of attitude response on the trajectory dynamics. This simulation terminates at TAEM-autoland interface.
Shuttle Program. Mcc Level C Formulation Requirements: Shuttle Taem Guidance and Flight Control
1980
86 pages
Report
Keine Angabe
Englisch
Astronautics , Manned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Automatic flight control , Computer programs , Entry guidance (Sts) , Space shuttle orbiters , Terminal area energy management , Angle of attack , Automatic pilots , Degrees of freedom , Dynamic pressure , Reentry trajectories , Rotating bodies