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Non-Linear Space Stabilization System Acquiring Minimum Rate in Minimum Time With Minimum Energy

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1 Author(s)
Ray W. Bailey ; Missile Systems Division Atlantic Research Corporation Duarte, California

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.

Published in:

IEEE Transactions on Aerospace and Navigational Electronics  (Volume:Technical_Paper ,  Issue: 0 )