This chapter contains sections titled:
Introduction
Attitude Control Plant
Closed‐Loop Attitude Control
Roll Control System
Pitch Control of Rockets
Yaw Control of Rockets
Summary
Exercises
Reference
Attitude Control of Rockets
2011-07-15
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
guidance and control system ‐ for a rocket , attitude control of rockets ‐ for launch vehicle, aerodynamic load consideration , roll control system of launch vehicle ‐ reaction jet controlled, single‐axis spacecraft , pitch control of rockets ‐ pitch and yaw control of launch vehicle, and zero angle of attack , launch vehicle, operation ‐ speeds and altitudes , attitude control plant, of a rocket ‐ and zero angle of attack and sideslip , aerodynamic parameters ‐ for gravity‐turn rocket's pitch dynamics plant , pitch‐yaw aerodynamic symmetry ‐ by launch vehicles, and ballistic missiles , yaw control of rockets ‐ a feedforward path, not required in yaw control , closed‐loop attitude control ‐ feedback stabilization, for launch vehicles
Attitude control systems for sounding rockets
AIAA | 1970
|ATTITUDE CONTROL FOR SPINNING SOUNDING ROCKETS
AIAA | 1967
|Attitude Control Systems for Sounding Rockets
NTIS | 1967
|Attitude control system for sounding rockets Patent
NTRS | 1966
|