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Iterative Model Predictive Control for automatic carrier landing of carrier-Based Aircrafts Under Complex Surroundings and Constraints

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Journal of Shanghai Jiaotong university(Science) 2024年第4期29卷 712-724页

作者： ZHANG Xiaotian HE Defeng LIAO Fei College of Information Engineering Zhejiang University of TechnologyHangzhou310023China Aerospace Technology Institute China Aerodynamics Research and Development CenterMianyang621000SichuanChina

This paper considers the automatic carrier landing problem of carrier-based aircrafts subjected to constraints,deck motion,measurement noises,and unknown *** iterative model predictive control(MPC)strategy with constraints is proposed for automatic landing control of the ***,the long short-term memory(LSTM)neural network is used to calculate the adaptive reference trajectories of the *** the Sage-Husa adaptive Kalman filter and the disturbance observer are introduced to design the composite ***,an iterative optimization algorithm is presented to fast solve the receding horizon optimal control problem of MPC based on the Lagrange’s ***,some sufficient conditions are derived to guarantee the stability of the landing system in a closed loop with the ***,the simulation results of F/A-18A aircraft show that compared with the conventional MPC,the presented MPC strategy improves the computational efficiency by nearly 56%and satisfies the control performance requirements of carrier landing.

关键词： automatic carrier landing model predictive control(MPC) long short-term memory(LSTM)neural network stability computational efficiency

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Guidance and Control Techniques of carrier-Based Aircraft for automatic carrier landing

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Transactions of Nanjing University of Aeronautics and Astronautics 2017年第6期34卷 600-608页

作者： Zhen Ziyang Zhang Zhibin Zhang Junhong College of Automation Engineering Nanjing University of Aeronautics and AstronauticsNanjing 210016P.R.China Shenyang Aireraft Design and Research Institute Shenyang 110000P.R.China Xi'an Aircraft Design and Research Institute Xi'an 710000P.R.China

We summarize the guidance and control techniques of automatic carrier landing for carrier-based ***,we analyze the carrier landing operations of the manned fixed-wing aircraft,unmanned fixed-wing aircraft and ***,we look into the navigation and guidance system and the flight control methods for current different ***,we draw several conclusions of the development prospects for aircraft carrier landing,including the precision landing control techniques,precision approach and landing guidance techniques,and adaptive,reconfigurable and intelligent flight control techniques.

关键词： carrier-based aircraft automatic carrier landing guidance flight control

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H_∞ Preview Control for automatic carrier landing

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Transactions of Nanjing University of Aeronautics and Astronautics 2019年第6期36卷 919-926页

作者： FARHAN Masood XUE Yixuan' ZHEN Ziyang YANG Liuqing College of Automation Engineering Nanjing University of Aeronautics and AstronauticsNanjing 211106P.R.China Jiangsu Key Laboratory of Internet of Things and Control Technologies Nanjing 210016P.R.China

This paper focuses on the application of H_∞preview control in automatic carrier landing system(ACLS)for carrier-based *** to the mutual movement between aircraft and carrier,the landing process becomes considerably more challenging compared to a conventional runway *** systems mitigate this by predicting deck motion and generating ideal glide slope path for ***,this predicted glide slope information is available in advance,conventional control structures are still unable to use this future information.H_∞preview control has the ability to utilize this future information for improving tracking response and disturbance *** process of incorporating preview information into ACLS framework and synthesizing the H_∞preview controller is *** methodology is verified using the example of F/A-18 automatic carrier landing problem and results are presented.

关键词： H∞control preview control carrierbased aircraft automatic carrier landing robust preview control

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Research on the Technology of Information Fusion for the Redundancy Guidance for Aircraft automatic carrier landing

Research on the Technology of Information Fusion for the Red...

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第40届中国控制会议

作者： Wenzhe Wang Mingwei Lv Yaotong Yang Shaoqing Zhang Jinwen Hu AVIC Shenyang Aircraft Design & Research Institute Integrated Avionics Department Northwestern Polytechnical University Key Laboratory of Information Fusion Technology

Under the background of the application of the redundancy guidance for aircraft automatic carrier landing,aiming at the different degrees of transmission delay caused by the different working environments of multiple sensors,the current period data is predicted and estimated to achieve the time stamp calibration in this *** algorithm of Kalman sliding window filter fusion and the algorithm of covariance weighted fusion have been combined to unify the different processing methods in the different application scenarios in this *** experiments prove that the algorithm of information fusion which is optimized and improved has the ability of high precision,stability and anti-interference,and can deal with emergencies caused by the external environment effectively.

关键词： automatic carrier landing Kalman sliding window filter fusion covariance weighted fusion target state estimation

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