The TAEM guidance and body rotational dynamics models required for the MCC simulation of the TAEM mission phase are defined. This simulation begins at the end of the entry phase and terminates at TAEM autoland interface. The logic presented is the required configuration for the first shuttle orbital flight (STS-1). The TAEM guidance is simulated in detail. The rotational dynamics simulation is a simplified model that assumes that the commanded rotational rates can be achieved in the integration interval. Thus, the rotational dynamics simulation is essentially a simulation of the autopilot commanded rates and integration of these rates to determine orbiter attitude. The rotational dynamics simulation also includes a simulation of the speedbrake deflection. The body flap and elevon deflections are computed in the orbiter aerodynamic simulation.
MCC Level C Formulation Requirements. Shuttle TAEM Guidance and Flight Control, STS-1 Baseline
1980
85 pages
Report
No indication
English
Astronautics , Manned Spacecraft , Computer programs , Flight control , Guidance (Motion) , Space shuttle orbiters , Space transportation system 1 flight , Terminal area energy management , Automatic pilots , Brakes (For arresting motion) , Ground tracks , Roll , Rotating bodies , Sequencing , Speed control