DocumentCode
486250
Title
A State Space Approach to Body Bending Compensation for Missile Autopilot Design
Author
Klabunde, Richard R.
Author_Institution
Naval Weapons Center, China Lake, California
fYear
1985
fDate
19-21 June 1985
Firstpage
341
Lastpage
344
Abstract
A state space approach to the design of a body bending compensator is presented. A simple model composed of a flexible mode and a rigid body mode (represented by a constant) is used as a model for an observer based body bending compensator. A robustness recovery technique is utilized to generate a compensator that is less sensitive to uncertainty in the body bending frequency. A comparison between this design approach and a standard notch filter is presented.
Keywords
Acceleration; Accelerometers; Aerodynamics; Equations; Frequency; Missiles; Servomechanisms; Stability; State-space methods; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1985
Conference_Location
Boston, MA, USA
Type
conf
Filename
4788630
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