Title :
Torque Coupled Bang Bang Attitude Control
Author :
Axelband, Elliot I.
fDate :
6/1/1965 12:00:00 AM
Abstract :
The properties of gas jet torque coupled attitude control in the design context of a coast phase attitude control system for a nonatmospheric planetary landing space vehicle are discussed.
Keywords :
Aerospace control; Aerospace electronics; Aircraft navigation; Attitude control; Brightness; Equations; Fuels; Sensor systems; Space vehicles; Sun;
Journal_Title :
Aerospace and Navigational Electronics, IEEE Transactions on
DOI :
10.1109/TANE.1965.4319324
