Load Relief Autopilot Analysis to Minimize Launch Vehicle Peak Thrust Vector Deflection Requirements
1968
42 pages
Report
Keine Angabe
Englisch
Navigation, Guidance, & Control , Space Launch Vehicles & Support Equipment , Automatic pilots , Deflection , Loads (forces) , Solid propellant rocket engines , Stability , Thrust vector control , Aerodynamic configurations , Attitude (inclination) , Equations of motion , Flight paths , Transfer functions , Voyager project , Wind (meteorology)
DSpace@MIT | 1976
|VERSATILE LAUNCH VEHICLE DIGITAL AUTOPILOT*
SAE Technical Papers | 1969
|