https://orcid.org/0000-0001-9560-9262
https://orcid.org/0000-0001-5327-824X
https://orcid.org/0000-0001-5002-1115
https://orcid.org/0000-0001-5041-8243
https://orcid.org/0000-0001-9560-9262
https://orcid.org/0000-0001-5327-824X
https://orcid.org/0000-0001-5002-1115
https://orcid.org/0000-0001-5041-8243
A guidance and control system is proposed for automatic carrier landing of an unmanned aerial vehicle (UAV). To this end, the position and attitude of the carrier is predicted by considering the sea state so that the UAV guidance loop can be compensated during the final approach phase. The landing kinematics and reference trajectory are determined using the predicted touchdown position. Nonlinear guidance and control laws are designed based on a sliding-mode control scheme to make the UAV robustly follow the reference trajectory.
Sliding Mode Guidance and Control for UAV Carrier Landing
IEEE Transactions on Aerospace and Electronic Systems ; 55 , 2 ; 951-966
01.04.2019
2809786 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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