A brief overview of the (DAP) Dynamic Autopilot is given. Results of the dynamic interaction study of the Orbiter with the General Dynamics Beam are presented. Preliminary results of the three degree of freedom payload parametric study are also presented.
Shuttle flight control and structure interaction
1983-04-01
Conference paper
No indication
English
Space Shuttle flight control system
NTRS | 1975
|Flight control rework studied for shuttle
Tema Archive | 1975
|Space shuttle digital flight control system
NTRS | 1976
|NTRS | 1978
|