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用于人机耦合振荡探测的操纵振荡特征确定 被引量：4

Determination of Control Characteristic for Detecting the Aircraft Pilot Coupling
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摘要 为了实现人机耦合振荡的在线探测,提出了适于实时计算的滑动窗口Fourier变换递推算法和与人机耦合振荡相关的飞机操纵振荡特征,并通过人机耦合振荡试飞数据的计算,分析了操纵振荡特征的合理、有效性。最后指出拟进一步开展的研究工作及建议。 This paper presents the real-time algorithm of recursive Fourier transform for preprocessing aircraft control/response signals and extracting methodology of aircraft control oscillation characteristic for fuzzy APC/PIO online detection. Through extracting from flight test data of the aircraft pilot coupling, the control oscillation characteristic parameters were analyzed to be reasonable and effectiveness. Finally, some suggestions were put forward to further research.
作者 田福礼 高正红 俞志刚
机构地区 西北工业大学航空学院 中国飞行试验研究院飞机所
出处 《飞行力学》 CSCD 北大核心 2005年第2期73-76,80,共5页 Flight Dynamics
关键词 飞机-驾驶员耦合 在线探测 操纵特征提取 回归Fourier变换 aircraft pilot coupling online detecting control oscillation characteristic extraction recursive Fourier transform
分类号 V212.1 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献3

  • 1Duane T McRuer. Aviation Safety and Pilot Control[M]. Washington D C: National Academy Press,1997.
  • 2田福礼,高正红.人机耦合振荡的研究现状与展望[J].飞行力学,2005,23(1):9-13. 被引量：6
  • 3Geffrey J Jeram,Prasad J V R. Fuzzy Logic Detector for Pilot Induced Oscillation [A]. Proceedings of the American Helicopter Society 59th Annual Forum[C].Phoenix, AZ, 2003.

二级参考文献5

  • 1National Research Council.Aviation Safety and Pilot Control:Understanding and Preventing Unfavorable Pilot-Vehicle Interactions[M].National Academy Press,Washington,D C,1997.
  • 2Holger Duda.Prediction of Category II Aircraft-Pilot Couplings New Experimental Results[R].AIAA-97-3499,1997.
  • 3Geffrey J Jeram,Prasad J V R.Fuzzy Logic Detector for Aircraft Pilot Coupling and Pilot Induced Oscillation[C].Presented at the American Helicopter Society 59th Annual Forum,2003.
  • 4Raimbault N,Fabre P.Probabilistic Neural Detector of Pilot Induced Oscillation[R].AIAA-2001-4353,2001.
  • 5Geffrey J Jeram,Prasad J V R.Tactile Avoidance Cueing for Pilot Induced Oscillation[R].School of Aerospace Engineering,Georgia Institute of Technology,Atlanta,Georgia,2003.

共引文献5

同被引文献19

  • 1Committee on the Effects of Aircraft pilot Coupling on Flight Safety. Aviation safety and pilot control[M]. Washion: National Academy Press, 1997:30-80.
  • 2Klyde D H, Mccruer D T, Myers T T. Unifield pilot-induced oscillaion theory[R]. WL-TR-96-3028, 1995.
  • 3Mamdani E H, Assilian S. An experiment in linguistic synthesis with a fuzzy logic controller[J], International Journal of Man-Machine Studies, 1975,7(1) :1-13.
  • 4Jeram G J, Prasad J V R. Fuzzy logic detector for pilot induced oscillation[C]//Proceedings of 59th Annual Forum of the American Helicopter Society. 2003:6-8.
  • 5Raimbault N, Fabre P. Probabilistic neural detector of pilot induced oscillations[R]. AIAA-2001-4353, 2001.
  • 6Geffrey J J, Prasad J V R. Fuzzy Logic Detector for Pilot Induced Oscillation [ C ]. Proceedings of the American Helicopter Society 59th Annual Forum,2003.
  • 7David G Mitchell, David H Klyde. Recommended prac- tices for exposing pilot-induced oscillations or tendencies in the development process[ R]. AIAA-2004-6810,2004.
  • 8Donald A Johnson. Suppression of pilot-induced oscillation [ R]. AFIT/GAE/ENY/01-1,2002.
  • 9Greory P Gitbreath. Prediction of pilot-induced oscillations (PIO) due to actuator rate limiting using the open-loop onset point (OLOP) criterion [ R ]. AFIT/GAE/ENY!O1 M02,2001.
  • 10Kamal M Shweyk. Application of new and stand pioh-in- duced oscillation anaylsis methods to flight test data of the C-17 trasport aircraft [ R]. AIAA-2007-6387,2007.

引证文献4

二级引证文献5

飞行力学
2005年 第2期

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