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The effects of redundant control inputs in optimal control 被引量:13

The effects of redundant control inputs in optimal control
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摘要 For a stabilizable system, the extension of the control inputs has no use for stabilizability, but it is important for optimal control. In this paper, a necessary and sufficient condition is presented to strictly decrease the quadratic optimal performance index after control input extensions. A similar result is also provided for H2 optimal control problem. These results show an essential difference between single-input and multi-input control systems. Several examples are taken to illustrate related problems.
出处 《Science in China(Series F)》 2009年第11期1973-1981,共9页 中国科学(F辑英文版)
基金 Supported by the National Natural Science Foundation of China (Grant Nos. 90916003, 60674093, 60874011) the Key Projects of Educational Ministry of China (Grant No. 107110)
关键词 redundant control optimal control Riccati equation Hamilton matrix redundant control, optimal control, Riccati equation, Hamilton matrix
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  • 1张曙光,高浩.推力矢量飞机操纵指令的协调分配[J].西北工业大学学报,1996,14(3):361-365. 被引量:8
  • 2高彦玺,王衍洋,金长江.推力矢量控制与飞机过失速机动仿真研究[J].飞行力学,1997,15(1):23-29. 被引量:11
  • 3[1]Buffington J M.Tailless aircraft control allocaton[R].AIAA-97-4281,1999.
  • 4[2]Reigelsperger W C,Banda S S.Nonlinear simulation of a modified F-16 with full-envelope control laws[J].Control Engineer Practice,1998,(6):309-320.
  • 5[3]Durham W C.Constrained control allocation[J].Journal of Guidance,Control and Dynamics,1993,16(4):717-725.
  • 6[4]Kevin R S,Durham W C.A comparison of control allocation methods for the F-15 ACTIVE research aircraft utilizing real-time piloted simulations[R].AIAA-99-4281,1999.
  • 7[5]Reigelsperger W C,Banda S S.Nonlinear simulation of a modified F-16 with full-envelope control laws[J].Control Engineer Practice,1998,(6):309-320.
  • 8[6]Raney D L,Montgomery R C.Flight control using distributed shape-change effector arrays[R].AIAA-2000-1560,2000.
  • 9Raney D L, Montgomery R C. Flight Control Using Distributed Shape-Change Effector Arrays [R]. AIAA-2000-1560,2000.
  • 10Reigelsperger W C,Banda S S. Nonlinear Simulation of a Modified F-16 with Full-Envelope Control Laws [J]. Control Engineer Practice, 1998,17(6) :309-320.

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