[1]
|
Meyer G, Su R, Hunt L R. Application of nonlinear transformations to automatic flight control. Automatica, 1984, 1(20): 103−107
|
[2]
|
Lane S H, Stengel R F. Flight control design using nonlinear inverse dynamics. Automatica, 1988, 24(4): 471−483 doi: 10.1016/0005-1098(88)90092-1
|
[3]
|
Daniel J B, Dale F E. Nonlinear control law with application to high angle-of-attack flight. Journal of Guidance, Control and Dynamics, 1992, 15(3): 761−767 doi: 10.2514/3.20902
|
[4]
|
Snell S A, Nns D F, Arrard W L. Nonlinear inversion flight control for a supermaneuverable aircraft. Journal of Guidance, Control, and Dynamics, 1992, 15(4): 976−984 doi: 10.2514/3.20932
|
[5]
|
Da Costa R R, Chu Q P, Mulder J A. Reentry flight controller design using nonlinear dynamic iversion. Journal of Spacecraft and Rockets, 2003, 40(1): 64−71 doi: 10.2514/2.3916
|
[6]
|
Roenneke A, Well K. Nonlinear flight control for a high-lift reentry vehicle. In: Proceedings of Guidance, Navigation, and Control Conference. Munich, Germany, 1995: 1798−1805
|
[7]
|
Luca A D, Lucibello P, Ulivi A G. Inversion techniques for trajectory control of flexible robotarms. Journal of Robotic Systems, 1989, 6(4): 325−344 doi: 10.1002/rob.4620060403
|
[8]
|
Furuta K, Okutani T, Sone H. Computer cont-rol of a double inverted pendulum. Computer & Electrical Engineering, 1978, 5(1): 67−84
|
[9]
|
Hatakeyama N, Shimada A. Movement control using zero dynamics of two-wheeled inverted pendulum robot. IEEE International Workshop on Advanced Motion Control, 2013, 44(3): 38−43
|
[10]
|
Enns D, Bugajski D, Hendrick R. Dynamic inversion: an evolving methodology for flight control design. International Journal of control, 1994, 59(1): 71−91 doi: 10.1080/00207179408923070
|
[11]
|
Joshua H, John V. Direct L1 adaptive nonlinear dynamic inversion control for command augmentation systems. In: Proceedings of Guidance, Navigation, and Control Conference and Exhibit. Kissimmee, Florida, USA: AIAA, 2018.
|
[12]
|
Geiser M, Xargay E, Hovakimyan N, Bierling T, Holzapfel F. L1 adaptive augmented dynamic inversion controller for a high agility UAV. In: Proceedings of Guidance, Navigation, and Control Conference, Portland, Oregon, USA: AIAA, 2011.
|
[13]
|
Yang I, Kim D, Lee D. A flight control strategy using robust dynamic inversion based on sliding mode control. In: Proceedings of Guidance, Navigation, and Control Conference and Exhibit. Mi-nneapolis, Minnesota, USA: AIAA, 2012.
|
[14]
|
Smith P. A simplified approach to nonlinear dynamic inversion based flight control. In: Proceedings of the 23rd Atmospheric Flight Mechanics Conference. Boston, USA: AIAA, 1998. 762−770
|
[15]
|
陈海兵, 张曙光, 方振平. 加速度反馈的隐式动态逆鲁棒非线性控制律设计. 航空学报, 2009, 30(4): 597−603 doi: 10.3321/j.issn:1000-6893.2009.04.003Chen Hai-Bing, Zhang Shu-Guang, Fang Zhen-Ping. Implitcit NDI robust nonlinear controldesign with acceleration feedback. ACTA Aeronautica et Astronautica Sinica, 2009, 30(4): 597−603 doi: 10.3321/j.issn:1000-6893.2009.04.003
|
[16]
|
Grondman F, Looye G H N, Kuchar R O, Chu Q P. Design and flight testing of incremental nonlinear dynamic inversion based control laws for a passenger aircraft. In: Proceedings of Guidance, Navigation, and Control Conference and Exhibit. Kissimmee, Florida, USA: AIAA, 2018.
|
[17]
|
Sieberking S, Chu Q P, Mulder J A. Robust flight control using incremental nonlinear dynamic inversion and angular acceleration prediction. Journal of Guidance Control and Dynamics, 2010, 33(6): 1732−1742 doi: 10.2514/1.49978
|
[18]
|
周池军, 朱纪洪. 考虑作动器动态补偿的飞机增量滤波非线性控制. 控制理论与应用, 2017, 34(5): 594−600 doi: 10.7641/CTA.2017.60402Zhou Chi-Jun, Zhu Ji-Hong. Incremental filte-red nonlinear control for aircraft with actuator dynamics compensation. Control Theory and Applications, 2017, 34(5): 594−600 doi: 10.7641/CTA.2017.60402
|
[19]
|
Slotine J J, Li W, Hall P. Applied Nonlinear Control. Englewood Cliffs, NewJersey: Prentice-Hall, Inc, 1991. 120−130
|
[20]
|
韩京清. 从PID技术到自抗扰控制技术. 控制工程, 2002, 9(3): 13−18 doi: 10.3969/j.issn.1671-7848.2002.03.003Han Jing-Qing. From PID technique to active disturbances rejection control technique. Control Engineering of China, 2002, 9(3): 13−18 doi: 10.3969/j.issn.1671-7848.2002.03.003
|