Title :
Non-Linear Space Stabilization System Acquiring Minimum Rate in Minimum Time With Minimum Energy
Author_Institution :
Missile Systems Division Atlantic Research Corporation Duarte, California
Abstract :
The efficient use of fuel and the rapid damping of disturbances are desirable in control systems. A system utilizing a derived control equation and modulation techniques is presented in Section I which meets these efficiency and damping requirements. Section II describes a second system in which displacement and rate-logic switching are separated to eliminate the hardware uncertainties that prove detrimental to switching line summing techniques.
Keywords :
Control systems; Damping; Displacement control; Equations; Fuels; Hardware; Limit-cycles; Logic; Nonlinear control systems; Space vehicles;
Journal_Title :
Aerospace and Navigational Electronics, IEEE Transactions on
DOI :
10.1109/TANE.1963.4502249
