Research on aerobraking guidance schemes is presented. The intent is to produce aerobraking guidance trajectories exhibiting many of the desirable characteristics of optimal aerobraking trajectories. Both one-control schemes and two-control schemes are studied. The research is in the interest of aeroassisted flight experiment vehicles (AFE) and aeroassisted orbital transfer (AOT) vehicles.
Guidance trajectories for aeroassisted orbital transfer
1990-01-01
Report
No indication
English
Guidance Trajectories for Aeroassisted Orbital Transfer
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