基于预定义时间的直接升力着舰增量控制

doi:10.7527/S1000-6893.2024.31163

Abstract

Abstract:

To address the disturbance of carrier wake and deck motion to carrier-based aircraft， this paper combines direct lift technology and incremental nonlinear control based on the predefined-time theory to improve the landing accuracy of carrier-based aircraft. Firstly， the full-state nonlinear dynamic equations of the aircraft are established， and the mechanisms and advantages of the direct lift control technology are analyzed. Secondly， an incremental control method based on the predefined-time theory is proposed， and an automatic landing controller for the carrier-based aircraft， consisting of the attitude stabilization loop， altitude control loop， and approach power compensation system， is designed based on this method. The designed automatic landing controller ensures that the tracking error of the carrier-based aircraft state converges to an adjustable bounded range within a predefined time， even under the influence of disturbances， thus enhancing its ability to rapidly track landing trajectory commands and deck movements. Moreover， this controller utilizes its robustness to reduce the impact of the carrier wake on the carrier-based aircraft. Subsequently， the predefined-time stability of the automatic landing closed-loop control system is rigorously proven under the Lyapunov stability theory. Finally， a series of real-time simulations verifies the effectiveness and superiority of the designed automatic landing controller.

Key words: direct lift-based carrier-based aircraft landing, predefined-time control, incremental nonlinear control, air wake suppression, nonlinear tracking differentiator

CLC Number:

V249.1

Yu LI, Tongwen CHEN, Zhigang WANG, Chiyung WEN, Xiaoxiong LIU. Incremental control of direct lift landing based on predefined-time theory[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(13): 531163.

Figures/Tables 8

Fig.1

Fig.2

Table 1

Parameters of predefined-time direct lift-based automatic landing controller

参数	数值	参数	数值	参数	数值
k₁	2	k₂	1.5	m/n	3
$λ$	30	R	55	$φ$	0.4
T_p1	6	T_p2，T_p5	0.1	T_p3	2
T_p4	12	T_p6	8	T_p7	5
a₁，a₂，a₅	1	b₁	1.2	b₂，b₅，b₇	1
a₃	2.2	b₃	2.5	a₄，a₇	1.8
b₄	2.3	a₆	1.4	b₆	2

Table 1

Fig.3

Fig.4

Fig.5

Fig.6

Fig.7

References 24

[1]	GREEN B E， FINDLAY D. CFD analysis of the F/A-18E super hornet during aircraft-carrier landing high-lift aerodynamic conditions‍［C］‍∥54th AIAA Aerospace Sciences Meeting. Reston： AIAA， 2017.
[2]	胡伟，万文章，陈谋. 基于神经网络和干扰观测器的UAV自动着舰控制［J］. 航空学报， 2022， 43（S1）： 72693.
	HU W， WAN W Z， CHEN M. Neural network and disturbance observer based control for automatic carrier landing of UAV‍［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（S1）： 726963 （in Chinese）.
[3]	DUAN H B， CHEN L， ZENG Z G. Automatic landing for carrier-based aircraft under the conditions of deck motion and carrier airwake disturbances‍［J］. IEEE Transactions on Aerospace and Electronic Systems， 2022， 58（6）： 5276-5291.
[4]	ZHANG Y， WU W H， WANG J， et al. Prescribed performance adaptive constrained backstepping controller for carrier-based longitudinal landing with magnitude constraints‍［C］‍∥2017 36th Chinese Control Conference （CCC）. Piscataway： IEEE Press， 2017： 856-861.
[5]	WANG L P， YUAN D H， CAO R T， et al. Automatic landing of carrier-based aircraft based on a collaboration of fault reconstruction and fault-tolerant control［J］. Aerospace Science and Technology， 2024， 144： 108772.
[6]	LI Y， LIU X X， ZHAO H， et al. Design of control law for Carrier-based Aircraft based on Ll adaptive control［C］∥2018 IEEE CSAA Guidance， Navigation and Control Conference （CGNCC）. Piscataway： IEEE Press， 2018： 1-6.
[7]	DENHAM J W. Project MAGIC CARPET： Advanced controls and displays for precision carrier landings‍［C］‍∥54th AIAA Aerospace Sciences Meeting. Reston： AIAA， 2016： 1770.
[8]	吴文海，汪节，高丽，等. MAGIC CARPET着舰技术分析［J］. 系统工程与电子技术， 2018， 40（9）： 2079-2091.
	WU W H， WANG J， GAO L， et al. Analysis on MAGIC CARPET carrier landing technology‍［J］. Systems Engineering and Electronics， 2018， 40（9）： 2079-2091 （in Chinese）.
[9]	段卓毅，王伟，耿建中，等. 舰载机人工进场着舰精确轨迹控制技术［J］. 航空学报， 2019， 40（4）： 622328.
	DUAN Z Y， WANG W， GENG J Z， et al. Precision trajectory manual control technologies for carrier-based aircraft approaching and landing［J］. Acta Aeronautica et Astronautica Sinica， 2019， 40（4）： 622328 （in Chinese）.
[10]	罗飞，张军红，王博，等. 基于直接升力与动态逆的舰尾流抑制方法［J］. 航空学报， 2021， 42（12）： 124770.
	LUO F， ZHANG J H， WANG B， et al. Air wake suppression method based on direct lift and nonlinear dynamic inversion control‍［J］. Acta Aeronautica et Astronautica Sinica， 2021， 42（12）： 124770 （in Chinese）.
[11]	何胜涛，江驹，余朝军，等. 基于自适应固定时间的直接升力着舰容错控制［J］. 电光与控制， 2023， 30（9）： 29-35， 98.
	HE S T， JIANG J， YU C J， et al. Fault-tolerant control of direct lift carrier landing based on adaptive fixed time［J］. Electronics Optics & Control， 2023， 30（9）： 29-35， 98 （in Chinese）.
[12]	孙笑云，江驹，甄子洋，等. 舰载飞机自适应模糊直接力着舰控制［J］. 西北工业大学学报， 2021， 39（2）： 359-366.
	SUN X Y， JIANG J， ZHEN Z Y， et al. Adaptive fuzzy direct lift control of aircraft carrier-based landing‍［J］. Journal of Northwestern Polytechnical University， 2021， 39（2）： 359-366 （in Chinese）.
[13]	柳仁地，江驹，张哲，等. 基于强化学习的舰载机着舰直接升力控制技术［J］. 北京航空航天大学学报， doi： 10.13700/j.bh.1001-5965.2023.0403 .
	LIU R D， JIANG J， ZHANG Z， et al. Direct lift control technology of carrier aircraft landing based on reinforcement learning‍［J］. Journal of Beijing University of Aeronautics and Astronautics， doi： 10.13700/j.bh.1001-5965.2023.0403 （in Chinese）.
[14]	郭锁凤. 先进飞行控制系统［M］. 北京：国防工业出版社， 2003： 207-210.
	GUO S F. Advanced flight control system［M］. Beijing： National Defense Industry Press， 2003： 207-210 （in Chinese）.
[15]	WU C H， YAN J G， SHEN J H， et al. Predefined-time attitude stabilization of receiver aircraft in aerial refueling［J］. IEEE Transactions on Circuits and Systems Ⅱ‍： Express Briefs， 2021， 68（10）： 3321-3325.
[16]	YE D， ZOU A M， SUN Z W. Predefined-time predefined-bounded attitude tracking control for rigid spacecraft［J］. IEEE Transactions on Aerospace and Electronic Systems， 2022， 58（1）： 464-472.
[17]	XIE S Z， CHEN Q. Adaptive nonsingular predefined-time control for attitude stabilization of rigid spacecrafts［J］. IEEE Transactions on Circuits and Systems Ⅱ‍： Express Briefs， 2022， 69（1）： 189-193.
[18]	NI J K， LIU L， LIU C X， et al. Fixed-time dynamic surface high-order sliding mode control for chaotic oscillation in power system［J］. Nonlinear Dynamics， 2016， 86（1）： 401-420.
[19]	WU Z J， XIA Y Q， XIE X J， et al. Stochastic Barbalat’s Lemma and Its Applications［J］. IEEE Transactions on Automatic Control， 2012， 57（6）： 1537-1543.
[20]	Tian D P， SHEN H H， DAI M. Improving the rapidity of nonlinear tracking differentiator via feedforward‍［J］. IEEE Transactions on Industrial Electronics， 2014， 61（7）： 3736-3743.
[21]	YANG H J， CHENG L， ZHANG J H， et al. Leader–follower trajectory control for quadrotors via tracking differentiators and disturbance observers［J］. IEEE Transactions on Systems， Man， and Cybernetics： Systems， 2021， 51（1）： 601-609.
[22]	LI Y， LIU X X， MING R C， et al. Improved model reference-based adaptive nonlinear dynamic inversion for fault-tolerant flight control‍［J］. International Journal of Robust and Nonlinear Control， 2023， 33（17）： 10328-10359.
[23]	LI Y， LIU X X， LU P， et al. Angular acceleration estimation-based incremental nonlinear dynamic inversion for robust flight control‍［J］. Control Engineering Practice， 2021， 117： 104938.
[24]	POLLACK T， VAN KAMPEN E J. Robust stability and performance analysis of incremental dynamic-inversion-based flight control laws‍［J］. Journal of Guidance， Control， and Dynamics， 2023， 46（9）： 1785-1798.

Incremental control of direct lift landing based on predefined-time theory

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 8

References 24

Related Articles 3

Recommended Articles

Metrics

Comments

[1]	Shihao XU, Yingzi GUAN, Jialun PU, Changzhu WEI. Predefined-time sliding mode control for VTHL launch vehicle in reentry phase [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 326857-326857.
[2]	Hongzhu ZHANG, Dong YE, Zhaowei SUN. Predefined-time integrated pose control for spacecraft under input quantization [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 328558-328558.
[3]	LUO Fei, ZHANG Junhong, WANG Bo, TANG Ruilin, TANG Wei. Air wake suppression method based on direct lift and nonlinear dynamic inversion control [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124770-124770.