Abstract
AbstractThis 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.KeywordsNonlinear dynamic inversionDirect lift controlPrecision landingCarrier-based fighter
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
