This paper proposes a control structure of the carrier-based fighter precision landing, which involves nonlinear dynamic inversion and direct lift control. This structure can eliminate the complex coupling of attitude and trajectory motion and quickly correct flight path deviation. The longitudinal nonlinear dynamics of the carrier-based fighter are established, and the dynamic inverse controllers for flight path angle loop, attitude loop, and velocity loop of the carrier-based fighter are constructed. Direct lift control is achieved through the control allocation of the stabilators, leading edge flaps, and trailing edge flaps, by which the force and moment are decoupled. The simulation results show that the state responses are rapid enough to reduce the landing track deviation.
Carrier-Based Fighter Precision Landing Based on Dynamic Inversion and Direct Lift Control
Lect. Notes Electrical Eng.
International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022
2023-01-31
10 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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