Prescribed performance adaptive constrained backstepping controller for carrier-based longitudinal landing with magnitude constraints

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• 英文论文题名：Prescribed performance adaptive constrained backstepping controller for carrier-based longitudinal landing with magnitude constraints
• 论文作者：Yang Zhang ; Wenhai Wu ; Jie Wang ; Li Gao
• 英文论文作者：Yang Zhang ; Wenhai Wu ; Jie Wang ; Li Gao ; Qingdao Branch ; Naval Aeronautical and Astronautical University
• 年：2017
• 作者机构：Qingdao Branch,Naval Aeronautical and Astronautical University;
• 英文论文关键词：Constrained Command filtered ; Prescribed Performance method ; Carrier-based landing ; longitude control
• 会议召开时间：2017-07-26
• 会议录名称：第36届中国控制会议论文集（A）
• 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
• 语种：英文
• 分类号：V271.492
• 学会代码：KZLL
• 会议名称：第36届中国控制会议
• 会议地点：中国辽宁大连
• 主办单位：中国自动化学会控制理论专业委员会
• 学会名称：中国自动化学会控制理论专业委员会
• 页数：6
• 文件大小：2206k
• 原文格式：D
• 会议级别：全国

摘要

The importance of carrier-based landing has been a controversial topic. The wave excites the ship to make six-degree-of-freedom motion, accompanied by atmosphere turbulence flow and ship airwake, making the carrier-based aircraft landing a great challenge. Aimed to ensure the safety of carrier-based aircraft and precision landing, a method of the constrained command filtered prescribed performance(CCFPP) is presented and applied to longitudinal landing. The proposed method in this paper has the following advantages. Firstly, the objectives of the approach are to stabilize the aircraft dynamics and to achieve accurate command landing track considering magnitude, rate, and bandwidth constraints on the aircraft states and the actuator. Secondly, in order to provide robustness to aerodynamic uncertainties, adaptive laws are designed to estimate unknown parameters of the model. Finally, another novel aspect of this approach is that not only analyzing the landing steady performance but also the transient performance, such as overshoot and convergence time. Lyapunov stability analysis and simulation demonstrations of the achieved performance are included.
The importance of carrier-based landing has been a controversial topic. The wave excites the ship to make six-degree-of-freedom motion, accompanied by atmosphere turbulence flow and ship airwake, making the carrier-based aircraft landing a great challenge. Aimed to ensure the safety of carrier-based aircraft and precision landing, a method of the constrained command filtered prescribed performance(CCFPP) is presented and applied to longitudinal landing. The proposed method in this paper has the following advantages. Firstly, the objectives of the approach are to stabilize the aircraft dynamics and to achieve accurate command landing track considering magnitude, rate, and bandwidth constraints on the aircraft states and the actuator. Secondly, in order to provide robustness to aerodynamic uncertainties, adaptive laws are designed to estimate unknown parameters of the model. Finally, another novel aspect of this approach is that not only analyzing the landing steady performance but also the transient performance, such as overshoot and convergence time. Lyapunov stability analysis and simulation demonstrations of the achieved performance are included.

引文

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