民机四维航迹/姿态一体化自适应控制

doi:10.7527/S1000-6893.2019.22437

Abstract

Abstract: Considering operating efficiency and flight safety, it is necessary to reduce the Total System Error (TSE) to improve the airspace resource utilization in the terminal area of the air route. During this route segment, Flight Technology Error (FTE) is the main composition. By proposing guidance and control integration design according to accurate tracking problem of four-dimensional trajectory during take-off and landing stage to reduce the flight technology error effectively. Considering the atmosphere turbulence, Loop Transfer Recovery (LTR) has been used to design state observer and optimal control and has realized the flight controller of civil aircraft. Based on that, the adaptive projection operator has been used to estimate the aerodynamic parameter uncertainties in inhomogeneous wind field and the uncertainties have been compensated. Numerical simulations demonstrate that the adaptive controller based on Linear Quadratic Gaussian/Loop Transfer Recovery (LQG/LTR) control technology can restrain the effect caused by uncertainty of aerodynamic parameters and atmospheric turbulence, and an integration controller of four-dimensional trajectory and attitudes for civil aircraft has been achieved.

Key words: future air navigation systems, performance based navigation, flight technology error, trajectory control, integration control, adaptive control

CLC Number:

V249.122

FAN Yao, SHAO Xingyue, LI Qingdong, REN Zhang. Integrated 4D trajectory and attitude adaptive controller for civil aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(2): 522437-522437.

References

[1] PETER D S, KARL R H, CHARLES A S. Validation of an integrated flight and propulsion control design for fighter aircraft[C]//23rd Joint Propulsion Conference. Reston, VA:AIAA, 1987:1928.
[2] LAMBERT H H, GILYARD G B, CHISHOLM J D, et al. Preliminary flight evaluation of an engine performance optimization algorithm[C]//27th Joint Propulsion Conference. Reston, VA:AIAA, 1991:1998.
[3] SMITH R H, CHISHOLM J D, STEWART J F. Optimizing aircraft performance with adaptive integrated flight/propulsion control[J]. Journal of Engineering for Gas Turbines and Power, 1991, 113(1):87-94.
[4] WILLIAMS D E, RICHMAN J, FRIEDLAND B. Design of an integrated strapdown guidance and control system for a tactical missile[C]//AIAA Guidance and Control Conference. Reston, VA:AIAA, 1983:2169.
[5] IDAN M, SHIMA T. Integrated sliding mode guidance and control for a missile with on-off actuators[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(4):1081-1089.
[6] SHTESSEL Y B, SHKOLNIKOV I A, LEVANT A. Guidance and control of missile interceptor using second-order sliding modes[J]. IEEE Transactions on Aerospace and Electronic Systems, 2009, 45(1):110-124.
[7] KIM B S, CALISE A J, SATTIGERI R. Adaptive integrated guidance and control design for line-of-sight based formation flight[J]. Journal of Guidance, Control, and Dynamic, 2007, 30(5):1386-1398.
[8] KIM B, KIM J, KIM B, et al. Adaptive integrated guidance and control design for automatic landing of a fixed wing unmanned aerial vehicle[J]. Journal of Aerospace Engineering, 2012, 25(4):490-500.
[9] SHARMA M, RICHARDS N. Adaptive integrated guidance and control for missile interceptors[C]//AIAA Guidance Navigation and Control Conference and Exhibit. Reston, VA:AIAA, 2004:4880.
[10] MENON K, OHLMEYER E J. Integrated design of agile missile guidance and autopilot systems[J]. Control Engineering Practice, 2001(9):1095-1106.
[11] MENON K, OHLMEYER E J. Nonlinear integrated guidance-control laws for homing missiles[C]//AIAA Guidance Navigation and Control Conference and Exhibit. Reston, VA:AIAA, 2001:4160.
[12] MENON K, OHLMEYEN E J. Optimal fixed-interval integrated guidance-control laws for hit-to-kill missiles[C]//AIAA Guidance Navigation and Control Conference and Exhibit. Reston, VA:AIAA, 2003:5579.
[13] 张杨, 吴文海, 汪杰. 舰载无人机横侧向着舰控制律设计[J]. 航空学报, 2017, 38(S1):721489. ZHANG Y, WU W H, WANG J. Design of carrier UAV lateral/directional landing control law[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(S1):721489(in Chinese).
[14] TIAN Y, LI Y, REN Z. Vision-based adaptive guidance law for intercepting a manoeuvring target[J]. IET Control Theory & Applications, 2011, 5(3):421-428.
[15] CHOI H, KIM Y. UAV guidance using a monocular-vision sensor for aerial target tracking[J]. Control Engineering Practice, 2014, 22(1):10-19.
[16] MEHTA S S, TON C, KAN Z, et al. Vision-based navigation and guidance of a sensorless missile[J]. Journal of the Franklin Institute, 2015, 352(12):5569-5598.
[17] WEN L, TAO G, YANG H, et al. Aircraft turbulence compensation using adaptive multivariable disturbance rejection techniques[J]. Journal of Guidance, Control, and Dynamics, 2014, 38(5):954-962.
[18] 肖业伦, 金长江. 大气扰动中的飞行力学[M]. 北京:国防工业出版社, 1991:11-89. XIAO Y L, JIN C J. Flight dynamics in atmospheric disturbance[M]. Beijing:National Defense Industry Press, 1991:11-89(in Chinese).
[19] 肖业伦. 飞行器运动方程[M]. 北京:航空工业出版社, 1987:62-89. XIAO Y L. Kinematic equation of aviation aircraft[M]. Beijing:Aviation Industry Press, 1987:62-89(in Chinese).
[20] 秦永元. 卡尔曼滤波与组合导航原理[M]. 西安:西北工业大学出版社, 2012:170-175. QIN Y Y. Theory of Kalman filter and integrated navigation[M]. Xi'an:Northwestern Polytechnical University Press, 2012:170-175(in Chinese).
[21] DOYLE J C. Guaranteed margins for LQG regulators[J]. IEEE Transactions on Automatic Control, 1978, 23(4):756-757.
[22] DOYLE J C, STEIN G. Multivariable feedback design:Concepts for a classical/modern synthesis[J]. IEEE Transactions on Automatic Control, 1981, 26(1):4-16.
[23] RIDGELY D B, BANDA S S, MCQUADE T E, et al. Linear-quadratic-gaussian with loop-transfer recovery methodology for an unmanned aircraft[J]. Journal of Guidance, Control, and Dynamics, 1987, 10(1):82-89.
[24] ZHOU K, REN Z. A new controller architecture for high performance robust and fault-tolerant Control[J]. IEEE Transactions on Automatic Control, 2001, 46(10):1613-1618.
[25] 韩京清. 自抗扰控制技术[M]. 北京:国防工业出版社, 2009:183-207. HAN J Q. Active disturbance rejection control technique[M]. Beijing:National Defense Industry Press, 2009:183-207(in Chinese).
[26] CHEN X, LI D H, GAO Z Q, et al. Tuning method for second-order active disturbance rejection control[C]//Proceedings of the 30th Chinese Control Conference. Piscataway, NJ:IEEE Press, 2011:6322-6327.
[27] 李杰, 齐晓慧, 夏元清, 等. 线性/非线性自抗扰切换控制方法研究[J]. 自动化学报, 2016, 42(2):202-212. LI J, QI X H, XIA Y Q, et al. On linear/nonlinear active disturbance rejection switching control[J]. Acta Automatica Sinica, 2016, 42(2):202-212(in Chinese).
[28] STEPANYAN V, HOVAKIMYAN N. Adaptive disturbance rejection controller for visual tracking of a maneuvering target[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(4):1090-1106.
[29] SASTRY S, BODSON M. Adaptive control:Stability, convergence and robustness[M]. Upper Saddle River, NJ:Prentice-Hall, 1989:18-19.

Integrated 4D trajectory and attitude adaptive controller for civil aircraft

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Fengying ZHENG, Zhimin SHEN, Yaqin LI, Kaizhao XU, Xinhua WANG. Gain adaptive multi-mode switching control for coaxial high-speed helicopter [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529088-529088.
[2]	Yuqing QIU, Yan LI, Jinxi LANG, Yuxian LIU, Zhong WANG. Robust adaptive attitude control of high-speed helicopters in transition mode [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529927-529927.
[3]	Kai NING, Baolin WU. Event-triggered-based orbit maintenance control for spacecraft subsatellite point control [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(10): 329412-329412.
[4]	Leyan FANG, Han MENG, Mingzhe HOU. Iterative learning sliding mode control with precise parameter estimation and its application [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628889-628889.
[5]	Guangquan DUAN, Guoping LIU. Adaptive prescribed control of position and attitude of combined spacecraft based on fully actuated system approach [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628837-628837.
[6]	Xiaoyun SUN, Shufan WU, Qiang SHEN. LMI-based output tracking robust drag-free control with model reference adaptive scheme [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727654-727654.
[7]	Runchang HU, Zian WANG, Yongliang CHEN, Dapeng ZHOU, Dapeng YANG, Zheng GONG. Stability augmentation control of thrust-vectored V/STOL aircraft based on L1 adaptive control [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727642-727642.
[8]	Chenyang LIU, Dawei WU, Yize GUO, Xinsai LV, Jiani ZHOU, Shuyi SHAO. Robust adaptive attitude control of quadrotor with uncertain strong coupling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727645-727645.
[9]	Yajie MA, Juan WANG, Bin JIANG, Jianye GONG. A fault⁃tolerant control scheme for UAVs-UGVs formation systems [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 327216-327216.
[10]	Feiyan GUO, Jianhua LIU, Qingdong XIAO, Shihong XIAO, Zhongqi WANG. Monitoring and evaluation of working condition and adaptive control technology for digital assembly tooling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(16): 427914-427914.
[11]	YANG Xiaowei, GE Yaowen, DENG Wenxiang, YAO Jianyong, ZHOU Ning. Active fault-tolerant control for hydraulic actuating cylinders of aeroengine guide vane control mechanisms [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 625464-625464.
[12]	WU Baohai, ZHANG Yang, ZHENG Zhiyang, ZHANG Ying, ZHANG Siqi. Review and prospects of feedrate optimization in CNC machining [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(4): 525467-525467.
[13]	SHI Zhongjiao, ZHU Huajie, ZHAO Liangyu, LIU Zhijie. Adaptive decoupling control for a class of spinning rockets considering actuator dynamics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 325068-325068.
[14]	ZHANG Pu, XUE Huifeng, GAO Shan. Distributed adaptive fault-tolerance consensus control for multi-agent system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 323539-323539.
[15]	ZHANG Jialong, YAN Jianguo, ZHANG Pu. Multi-UAV formation forming control based on adaptive method under wind field disturbances [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(1): 323385-323385.