Volume 28 Issue 3
Mar.  2002
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WANG Liang, LIN Yan-zhi, WANG Zhan-linet al. Flight Director Signal Synthesis for Landing Approach Operation Based on Optimal FCZPETC[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(3): 312-315. (in Chinese)
Citation: WANG Liang, LIN Yan-zhi, WANG Zhan-linet al. Flight Director Signal Synthesis for Landing Approach Operation Based on Optimal FCZPETC[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(3): 312-315. (in Chinese)

Flight Director Signal Synthesis for Landing Approach Operation Based on Optimal FCZPETC

  • Received Date: 25 Sep 2000
  • Publish Date: 31 Mar 2002
  • 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

     

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  • [1]Hess R A, Peter J G. Design and evaluation of cockpit display for hovering flight[J]. J Guidance, 1990,13(3):450~457. [2]McRuer D T, Weir D H, Klein R H. A pilot-vehicle systems approach to longitudinal flight director design[J]. J Guidance,1971,8(11):890~897. [3]Tomizuka M. Zero phase error tracking algorithm for digital control[J]. ASME J of Dynamic Systems, Measurement, and Control, 1987, 109:65~68. [4]Funahashi Y, Yamada M. Zero phase error tracking controllers with optimal gain characteristics[J]. ASME J of Dynamic Systems, Measurement, and Control, 1993, 115:311~318. [5]Yamada M, Funahashi Y, Fujiwara S. Zero phase error tracking systems with arbitrary specified gain characteristics[J]. ASME J of Dynamic Systems, Measurement, and Control, 1997, 119:260~264.
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