Dynamic inversion: an evolving methodology for flight control design
Author:
Affiliation:
1. a Honeywell Inc , MN-15-2321, SRC, 1625 Zaarthan Avenue, St. Louis Park, MN 55416, U.S.A.
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207179408923070
Reference26 articles.
1. Nonlinear control law with application to high angle-of-attack flight
2. Feedback Systems: Input-Output Properties
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