Dynamic inversion: an evolving methodology for flight control design
- 1 January 1994
- journal article
- research article
- Published by Taylor & Francis in International Journal of Control
- Vol. 59 (1) , 71-91
- https://doi.org/10.1080/00207179408923070
Abstract
This paper describes nonlinear dynamic inversion as an alternative design method for flight controls. The method is illustrated with super-manoeuvring control laws for the F-18 high angle-of-attack research vehicle.Keywords
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