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

WANG Liang; LIN Yan-zhi; WANG Zhan-lin

Volume 28 Issue 3

Mar. 2002

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Journal of Beijing University of Aeronautics and Astronautics > 2002 > 28(3): 312-315.

Huang Jun, Wu Zhe, Zhu Rongchanget al. Optimized Collocation of Combat Aircraft Weapon Systems for Air Force[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 546-549. (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)

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

1.
Beijing University of Aeronautics and Astronautics, School of Automation Science and Electrical Engineering
2. Shenyang Aircraft Corporation

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

Abstract

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
- flight director,
- flight control,
- gliding control,
- zero phase error tracking control

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References(1)

References

[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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沈阳化工大学材料科学与工程学院沈阳 110142

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