Ⅱ型PIO反馈与前馈抑制系统对比

Abstract

Abstract: When rate limiter is saturated, the additional time delay would occur. It could deteriorate aircraft flying quality and cause category Ⅱ pilot-induced-oscillations(PIO). The rate-limited feedback(RLF) and the dead area stability augmentation(DASA) schemes prevent the category Ⅱ PIO from occurring. The open loop phase compensation capability of two schemes is studied based on describing functions method. The parameter optimization method of RLF scheme is provided. The influence of deadzone and filter parameters on DASA scheme phase compensation capability is analyzed. The responses of two schemes to sine wave input and bias input are examined. The pilot-vehicle system model with rate limiter is developed. The generation mechanism of category Ⅱ PIO is analyzed and the expression to avoid category Ⅱ PIO is derived. The continuous signal phase compensation method is applied to preventing category Ⅱ PIO. The step, discrete and sine tracking tasks which are easy to induce PIO are simulated, and the prevention capabilities of two schemes are compared. The results demonstrate that the RLF scheme has better capability for avoiding category Ⅱ PIO and decreases the occurrence possibility of category Ⅱ PIO.

Key words: flight control systems, pilot induced oscillations, describing functions, actuators, rate-limit

CLC Number:

V212.1

Meng Jie;Xu Haojun;Zhang Jiankang. A Comparison of Feedback and Foreback Schemes to Prevent Category Ⅱ PIO[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(9): 1701-1707.

References

［1］Weltz 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. ［2］Alcala 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. ［3］Liebst 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. ［4］Brieger 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. ［5］Gatley S L, Turner M C, Postlethwaite I, et al. A comparison of rate-limit compensation schemes for pilot-induced-oscillation avoidance［J］. Aerospace Science and Technology, 2006, 10(1): 37-47. ［6］Katayanagi R. Pilot-induced oscillation analysis with actuator rate limiting and feedback control loop［C］ ∥AIAA Guidance, Navigation, and Control Conference. 2004: 1162-1168. ［7］李建平,杨朝旭,罗欣. 作动器速率饱和时的PIO抑制方法［J］. 航空学报, 2003, 24(3): 263-265. Li Jianping, Yang Zhaoxu, Luo Xin. Method to prevent pilot-induced-oscillations due to actuator rate limiting［J］. Acta Aeronautica et Astronautica Sinica, 2003, 24(3): 263-265. （in Chinese） ［8］Groot S, Pavel M D. New insights into pilot behaviour during hazardous rotorcraft pilot induced oscillations［C］ ∥Annual Forum - Vertical Flight: Leading Through Innovation - Proceedings. 2006: 1131-1142. ［9］孟捷, 徐浩军, 武卫. 驾驶员模型对Ⅱ型PIO预测影响研究［J］. 系统仿真学报, 2009, 21(12): 3816-3819. Meng Jie, Xu Haojun, Wu Wei. Research on prediction of category Ⅱ PIO affected by pilot model［J］. Journal of System Simulation, 2009, 21(12): 3816-3819. （in Chinese） ［10］James G. A comparison of nonlinear algorithms to prevent pilot-induced oscillations caused by actuator rate limiting［D］. Wright-Patterson AFB OH: Air Force Institute of Technology, 2003.

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A Comparison of Feedback and Foreback Schemes to Prevent Category Ⅱ PIO

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