运输机超低空重装空投抗侧风三维非线性控制律设计
收稿日期: 2013-10-10
修回日期: 2013-12-04
网络出版日期: 2013-12-14
基金资助
国家自然科学基金(61134004)
Design of Three Dimensional Nonlinear Controller for Transport Aircraft Airdropping Heavy Cargos at Extremely Low-altitude Under Crosswind
Received date: 2013-10-10
Revised date: 2013-12-04
Online published: 2013-12-14
Supported by
National Natural Science Foundation of China (61134004)
辛琪 , 史忠科 . 运输机超低空重装空投抗侧风三维非线性控制律设计[J]. 航空学报, 2014 , 35(7) : 1941 -1956 . DOI: 10.7527/S1000-6893.2013.0485
Large transport aircraft suffer from catastrophes and uncertainties in both longitudinal and lateral directions at the moment of airdropping heavy cargos at extremely low-altitude under a crosswind. A three dimensional nonlinear controller for transport aircraft airdropping cargos is investigated. Taking the crosswind and the ground effect into account, the airdropping dynamics including catastrophes and uncertainties is established. To ensure flight safety, a three dimensional controller is proposed by a fourth-order compound approach. The virtual commands for the position loop are given gradually to cause the errors of the position, the flight path and the attitude to propagate toward the inner loop. Subsequently, the control surface and the throttle setting are designed to eliminate the errors of both the position and air speed loops. The closed loop stability of the control system under weak uncertainties is analyzed. Simulations show that the proposed controller can ensure the flight safety for transport aircraft airdropping heavy cargos at extremely low-altitudes under a crosswind.
[1] Jann T. Coupled simulation of cargo airdrop from a generic K, Mani M, Sabzehparvar M, et al. A single heavy load airdrop and its effect on a reversible flight control system[J]. Aircraft Engineering and Aerospace Technology, 2008, 80(4): 400-407.
[3] Han Y H, Lu Y P. Dynamics analysis for transport airdropping heavy cargo at super-low-altitude and design of H∞ robust control[J]. Journa1 of Nanjing University of Aeronautics & Astronautics, 2012, 44(1): 75-80. (in Chinese) 韩艳铧, 陆宇平. 运输机超低空空投重物动力学分析与H∞鲁棒控制设计[J]. 南京航空航天大学学报, 2012, 44(1): 75-80.
[4] Tang Y M, Zhang W G, Liu B N. Design of longitudinal control system during airdrop based on adaptive dynamic inversion theory[J]. Computer Measurement & Control, 2011, 19(7): 1639-1642. (in Chinese) 唐一萌, 章卫国, 刘宝宁. 基于自适应逆的飞机空投纵向控制系统设计[J]. 计算机测量与控制, 2011, 19(7): 1639-1642.
[5] Zhang H Y, Shi Z K. Variable structure control of catastrophic course in airdropping heavy cargo[J]. Chinese Journal of Aeronautics, 2009, 22(5): 520-527.
[6] Li D D, Sun X X, Dong W H, et al. Pitch control for flight in heavy-weight airdrop based on feedback linearization theory and variable-structure control[J]. Control Theory & Applications, 2013, 30(1): 54-60. (in Chinese) 李大东, 孙秀霞, 董文瀚, 等. 基于线性化反馈的滑模变结构重装空投纵向控制律设计[J]. 控制理论与应用, 2013, 30(1): 54-60.
[7] Feng Y, Shi Z K, Tang W. Dynamics modeling and control of large transport aircraft in heavy cargo extraction[J]. Journal of Control Theory and Applications, 2011, 9(2): 231-236.
[8] Yang Y, Lu Y P. Backstepping sliding mode control for super-low altitude heavy cargo airdrop from transport plane[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(12): 2301-2312. (in Chinese) 杨雨, 陆宇平. 运输机超低空重装空投纵向反步滑模控制研究[J]. 航空学报, 2012, 33(12): 2301-2312.
[9] Chen J, Shi Z K. Flight controller design of transport airdrop[J]. Chinese Journal of Aeronautics, 2011, 24(5): 600-606.
[10] Yang Y, Lu Y P, Dai Z S. Counteracting crosswind controller design for low altitude heavy cargo airdrop based on dynamic inversion theory[J]. Flight Dynamics, 2013, 31(1): 37-41. (in Chinese) 杨雨, 陆宇平, 戴正升. 基于动态逆的超低空空投抗侧风控制器设计[J]. 飞行力学, 2013, 31(1): 37-41.
[11] Feng Y L, Shi Z K. Robust dynamic inversion control for cargo extraction during airdrop at super low attitude[J]. Control Engineering of China, 2010, 17(5): 579-583. (in Chinese) 冯艳丽, 史忠科. 超低空空投货物出舱过程的动态逆鲁棒控制[J]. 控制工程, 2010, 17(5): 579-583.
[12] Lee T, Kim Y. Nonlinear adaptive flight control using backstepping and neural networks controller[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(4): 675-682.
[13] Xu B, Sun F C, Liu H, et al. Adaptive Kriging controller design for hypersonic flight vehicle via back-stepping [J]. IET Control Theory and Applications, 2012, 6(4): 487-497.
[14] Chen J, Shi Z K. Aircraft modeling and simulation with cargo moving inside[J]. Chinese Journal of Aeronautics, 2009, 22(2): 191-197.
[15] Yang Y, Lu Y P. Dynamics modelling for super low attitude parachute extraction system on transport airplane[J]. Journa1 of Nanjing University of Aeronautics & Astronautics, 2012, 44(3): 294-300. (in Chinese) 杨雨, 陆宇平. 飞机超低空牵引空投动力学响应研究[J]. 南京航空航天大学学报, 2012, 44(3): 294-300.
[16] Li D D, Sun X X, Dong W H, et al. Improved heavy-weight airdrop model considering many influence factors[J]. Systems Engineering and Electronics, 2013, 35(2): 447-451. (in Chinese) 李大东, 孙秀霞, 董文瀚, 等.考虑多种影响因素下的改进重装空投系统建模[J]. 系统工程与电子技术, 2013, 35(2): 447-451.
[17] Garza F R. Morelli E A. A collection of nonlinear aircraft simulations in MATLAB, NASA/TM-2003-212145. Washington, D.C.: NASA, 2003.
[18] Adams R J, Buffington J M, Banda S S. Design of nonlinear control laws for high-angle-of-attack flight[J]. Journal of Guidance, Control, and Dynamics, 1994, 17(4): 737-746.
[19] Khalil H K. Nonlinear systems[M]. 3rd ed. Upper Saddle River: Prentice Hall, 2002: 553-627.
[20] Roskam J. Airplane flight dynamics and automatic flight controls[M]. Lawrence: Design, Analysis and Research Corporation, 2001: 543-549.
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