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New stabilization design for planar vertical take-off and landing aircrafts

New stabilization design for planar vertical take-off and landing aircrafts

作     者:Ye, Huawen Sheng, Liang Gui, Weihua Yang, Chunhua 

作者机构:School of Information Science and Engineering Central South University Changsha Hunan 410083 China 

出 版 物:《控制理论与应用(英文版)》 (JOURNAL OF CONTROL THEORY AND APPLICATIONS)

年 卷 期:2011年第9卷第2期

页      面:195-202页

核心收录:

学科分类:0711[理学-系统科学] 0808[工学-电气工程] 07[理学] 08[工学] 0835[工学-软件工程] 0802[工学-机械工程] 081101[工学-控制理论与控制工程] 0811[工学-控制科学与工程] 0812[工学-计算机科学与技术(可授工学、理学学位)] 071102[理学-系统分析与集成] 081103[工学-系统工程] 

基  金:supported by the National Natural Science Foundation of China (No. 60874008) the Research Fund for the Doctoral Program of High Education of China (No. 200805331102) 

主  题:Stabilization Planar vertical take-off and landing (PVTOL) Nonlinear control Saturated control 

摘      要:This paper presents a new stabilizing control law for a planar vertical take-off and landing *** model is first transformed into an equivalent form,and then a control law consisting of a linear term and a saturated term is given for a related subsystem,with the saturation levels being assigned as large as *** to the existing saturation scheme in which all states are restricted by saturations,the design brings about a relatively fast *** effectiveness and advantage of the design are validated by numerical simulations.

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