Torque Coupled Bang Bang Attitude Control

1 June 1965

journal article
Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace and Navigational Electronics

Vol. 12 (2), 129-133
https://doi.org/10.1109/TANE.1965.4319324

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

SPACE VEHICLES
SUN
AEROSPACE ELECTRONICS
AIRCRAFT NAVIGATION
FUELS
BRIGHTNESS
ATTITUDE CONTROL
SENSOR SYSTEMS
AEROSPACE CONTROL
EQUATIONS

Cited by 1 article