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�������պ����ѧѧ�� 2002, Vol. 28 Issue (3) :312-315    DOI:
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Flight Director Signal Synthesis for Landing Approach Operation Based on Optimal FCZPETC
WANG Liang1, LIN Yan-zhi2, WANG Zhan-lin1*
1. Beijing University of Aeronautics and Astronautics, School of Automation Science and Electrical Engineering;
2. Shenyang Aircraft Corporation

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Abstract�� Features of flight director design were analyzed. Considering the roles of preview information in improving pursuit flight property and compensating pilot's time delay, a new method for flight director signal synthesis with preview information was proposed based on zero phase error tracking control. Application features of the method and the improvement in approaching pursuit were demonstrated through simulation results
Keywords�� flight director   flight control   gliding control   zero phase error tracking control     
Received 2000-09-25;
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WANG Liang, LIN Yan-zhi, WANG Zhan-lin.Flight Director Signal Synthesis for Landing Approach Operation Based on Optimal FCZPETC[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2002,V28(3): 312-315
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2002/V28/I3/312
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