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运输机超低空空投下滑阶段PIO趋势评估与抑制 被引量:2

Evaluation and suppression of PIO tendency during ultra-low altitude airdrop of transport airplanes
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摘要 提出了超低空空投下滑阶段的PIO问题,研究了空投下滑拉平阶段产生PIO的主要原因。基于描述函数法分析了速率限制反馈(RLF)PIO抑制系统的相位补偿能力和PIO产生机理,推导了抑制PIO发生的计算公式。应用RLF连续信号相位补偿法抑制PIO的发生,对阶跃、离散和正弦三种易于诱发PIO现象的跟踪任务进行了数值仿真。结果表明,超低空空投下滑拉平阶段会发生PIO,严重威胁飞行安全,RLF对PIO具有较好的抑制效果。 The PIO problem in ultra-low altitude airdrop is put forward and the main causes of the PIO are analyzed. The phase compensation capability of RLF and mechanism of the PIO suppression are studied based on describing function method. The expression to prevent PIO is derived. The RLF phase compensating method is applied to avoid PIO. Step,discrete and sine tracking tasks are employed to study the suppression capability of the RLF suppresser in time domain simulation. The simulation results indicate when the rate limiter is saturated; the additional time delay might cause PIO during the ultra-low altitude airdrop process and threaten the safety of flight. The RLF suppresser works well in preventing the nonlinear PIO.
出处 《飞行力学》 CSCD 北大核心 2016年第1期26-30,共5页 Flight Dynamics
基金 国家自然科学基金资助(60904038) 航空科学基金资助(20141396012)
关键词 超低空空投 驾驶员诱发振荡 Neal-Smith准则 速率限制反馈抑制器 ultra-low altitude airdrop PIO Neal-Smith criterion RLF
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  • 1陈杰,史忠科.货物舱内移动过程的建模与仿真(英文)[J].Chinese Journal of Aeronautics,2009,22(2):191-197. 被引量:21
  • 2Feng, Yanli, Shi, Zhongke, Tang, Wei.Dynamics modeling and control of large transport aircraft in heavy cargo extraction[J].控制理论与应用(英文版),2011,9(2):231-236. 被引量:9
  • 3嵇鼎毅,陆宇平.飞翼布局无人机抗侧风自动着陆控制[J].飞机设计,2007,27(2):25-28. 被引量:6
  • 4张军红,李振水,詹孟权,高亚奎.LQG控制理论在阵风载荷减缓系统中的应用[J].飞行力学,2007,25(2):61-64. 被引量:21
  • 5布罗克豪斯.飞行控制[M].金长江译.北京:国防工业出版社,1999.
  • 6Weltz G, Shweyk K, Murray D. Application of new and standard pilot-induced oscillation (PIO) analysis methods to flight test data of the C-17 transport aircraft[C] ∥AIAA Atmospheric Flight Mechanics Conference.2007: 266-291.
  • 7Alcala I,Gordillo F, Aracil J. Phase compensation design for prevention of PIO due to actuator rate saturation[C] ∥Proceeding of the 2004 American Control Conference. 2004: 4678-4691.
  • 8Liebst B S, Chapa M, Leggett D. Nonlinear prefilter to prevent pilot-induced oscillations due to actuator rate limiting[J]. Journal of Guidance, Control, and Dynamics, 2002, 25(4): 740-747.
  • 9Brieger O, Kerr M, Leiling D,et al. Flight testing of a rate saturation compensation scheme on the ATTAS aircraft[J]. Aerospace Science and Technology, 2009, 13(2): 92-104.
  • 10Brieger O, Kerr M, Leiling D,et al. Flight testing of a rate saturation compensation scheme on the ATTAS aircraft[J]. Aerospace Science and Technology, 2009, 13(2): 92-104.

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