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再入滑翔飞行器控制系统鲁棒性能评估方法研究
  • ISSN号:1006-3242
  • 期刊名称:航天控制
  • 时间:2015
  • 页码:44-49+55
  • 分类:O231[理学—运筹学与控制论;理学—数学] TP13[自动化与计算机技术—控制科学与工程;自动化与计算机技术—控制理论与控制工程]
  • 作者机构:[1]School of Astronautics, Beihang University, Beijing 100083, China, [2]Science and Technology Committee, China Aerospace Science and Technology Corporation, Beijing 100048, China
  • 相关基金:This work was supported by the National Natural Science Foundation of China (Nos. 61174221 and 61402039).
  • 相关项目:近空间高速飞行器自适应多模型姿态控制研究
中文摘要:

To solve the receding horizon control(RHC) problem in an online manner, a novel numerical method called the indirect Radau pseudospectral method(IRPM) is proposed in this paper. Based on calculus of variations and the first-order necessary optimality condition, the RHC problem for linear time-varying(LTV) system is transformed into the two-point boundary value problem(TPBVP). The Radau pseudospectral approximation is employed to discretize the TPBVP into well-posed linear algebraic equations. The resulting linear algebraic equations are solved via a matrix partitioning approach afterwards to obtain the optimal feedback control law.For the nonlinear system, the linearization method or the quasi linearization method is employed to approximate the RHC problem with successive linear approximations. Subsequently, each linear problem is solved via the similar method which is used to solve the RHC problem for LTV system.Simulation results of three examples show that the IRPM is of high accuracy and of high computation efficiency to solve the RHC problem and the stability of closed-loop systems is guaranteed.

英文摘要:

To solve the receding horizon control (RHC) problem in an online manner, a novel numerical method called the indirect Radau pseudospectral method (IRPM) is proposed in this paper. Based on calculus of variations and the first-order necessary optimality condition, the RHC problem for linear time-varying (LTV) system is transformed into the two-point boundary value problem (TPBVP). The Radau pseudospectral approximation is employed to discretize the TPBVP into well-posed linear algebraic equations. The resulting linear algebraic equations are solved via a matrix partitioning approach afterwards to obtain the optimal feedback control law. For the nonlinear system, the linearization method or the quasi linearization method is employed to approximate the RHC problem with successive linear approximations. Subsequently, each linear problem is solved via the similar method which is used to solve the RHC problem for LTV system. Simulation results of three examples show that the IRPM is of high accuracy and of high compu- tation efficiency to solve the RHC problem and the stability of closed-loop systems is guaranteed.

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期刊信息
  • 《航天控制》
  • 北大核心期刊(2011版)
  • 主管单位:
  • 主办单位:北京航天自动控制研究所
  • 主编:齐春棠
  • 地址:北京142信箱402分箱
  • 邮编:100854
  • 邮箱:
  • 电话:010-68388585 68762264
  • 国际标准刊号:ISSN:1006-3242
  • 国内统一刊号:ISSN:11-1989/V
  • 邮发代号:80-338
  • 获奖情况:
  • 1987年航天系统科技期刊第二次评比中,被评为优秀...,1990年航天系统科技期刊第三次评比中,被评为优秀...
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  • 被引量:4120