Selection of desired dynamics for Dynamic Inversion controlled re-entry vehicles /

Dynamic Inversion is a design technique used to synthesize flight controllers whereby the set of existing plant dynamics are canceled out and replaced by a designer selected set of desired dynamics. The desired dynamics essentially form a loop-shaping compensator that affects the closed-loop respon...

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Bibliographic Details

Main Author:	Georgie, Jennifer Anne
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2001.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy