Three atmospheric guidance concepts proposed for an aeroassist flight experiment are presented. The flight experiment will simulate a return from geosynchronous orbit by an aeroassisted orbital transfer vehicle and is proposed to be flown on board the Space Shuttle in 1992. The three guidance concepts include an analytic predictor/corrector, a numeric predictor/corrector, and an energy controller. The algorithms for the three guidance methods are developed and performance results are presented for the nominal case and for several cases dispersed from the nominal conditions.
Atmospheric guidance concepts for an aeroassist flight experiment
1988-06-01
Sonstige
Keine Angabe
Englisch
Aeroassist flight experiment guidance Quiet Time
NTRS | 1988
|Aeroassist Flight Experiment (AFE)
NTRS | 1988
|The Aeroassist Flight Experiment
NTRS | 1987
|Aeroassist Flight Experiment (AFE)
NTIS | 1988
|