This paper is to present a robust controller design method for developing autonomous landing systems of Unmanned Combat Air Vehicle (UCAV). We first analyze the characteristic of autonomous landing of UCAV, and put forward its landing performance specifications. Structure singular value μ| synthesis is used to develop autonomous landing systems to accurately follow the pre-designed ideal landing track or online generated optimal landing track. The robust performance of system is analyzed. The simulation results demonstrate that the designed autonomous landing system satisfies the performance requirements of autonomous landing of UCAV when there are uncertainties of UCAV aircraft model, measurement noises and exogenous disturbances.
Research of autonomous landing control of unmanned combat air vehicle
Fifth International Symposium on Instrumentation and Control Technology ; 2003 ; Beijing,China
Proc. SPIE ; 5253
2003-09-02
Conference paper
Electronic Resource
English
Research of autonomous landing control of unmanned combat air vehicle [5253-162]
British Library Conference Proceedings | 2003
|Vision-based autonomous landing integrated navigation scheme of unmanned combat aerial vehicles
British Library Online Contents | 2007
|SYSTEM FOR AUTONOMOUS LANDING CONTROL OF UNMANNED AERIAL VEHICLE
European Patent Office | 2021
|Unmanned aerial vehicle autonomous dynamic landing device and landing method thereof
European Patent Office | 2023
|