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Nonlinear Autopilot Design for Aerospace Vehicles

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ISBN-10: 3639241207

ISBN-13: 9783639241204

Edition: N/A

Authors: Abhijit Das, Siddhartha Mukhopadhyay

List price: $8.00
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Description:

Traditionally, missile autopilots have been designed using linear control approaches with gain scheduling. Moreover, three single axis autopilots are usually designed without considering the interaction among the motion axes. Such designs cannot handle the coupling among pitch-yaw-roll channels, especially under high angles of attack occurring in high maneuver zones. In most research studies, realistic factors like fin saturation, limitation of gimbal freedom etc are not considered. Our research work contributed a nonlinear multivariable approach to the design of an autopilot for a realistic missile that overcomes these difficulties. At first, exact input-output (IO) feedback linearization…    
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Book details

List price: $8.00
Publisher: VDM Verlag Dr. Mueller e.K.
Binding: Paperback
Pages: 228
Size: 6.00" wide x 9.00" long x 0.52" tall
Weight: 0.748
Language: English