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《Ordnace Industry Automation》 2002-06
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The Design of Lateral Automatic Carrier Landing System Based on H-infinity Control

YUAN Suo-zhong, YANG Yi-dong (College of Automation, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China)  
The lateral automatic carrier landing system based on H-infinity control is that the performance specifications of typical control were translated into the weight array selection in H-infinity control using H-infinity technique. In virtue of requirements of lateral slide angle equaled to zero and restrained lateral wind for lateral automatic carrier landing system, the increment linear kinetic model, feedback controller and enhanced object model for selecting weight array coefficient were applied in synthesis design of H-infinity control, and the selective rule of weight array was deduced. The automatic landing system of F14 airplane was simulated, and simulation result shows that requirement of carrier landing and restrained lateral wind and excellent robustness has achieved the performance specifications of the design.
【CateGory Index】: V249.122
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