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多操纵面先进布局飞机控制分配技术研究 被引量:17

Control Allocation for High Performance Aircraft with Multi-Control Effectors
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摘要 介绍了多操纵面布局飞机飞控系统中冗余控制量分配问题的提出、数学描述及研究发展。重点分析了伪逆法、串接链法和基于二次规划的动态分配三种方法,通过某型先进布局飞机控制分配设计与仿真,对比分析了各种算法应用的优缺点,并给出了结论。 The control allocation problem for high performance aircraft with multi-control-effectors were introduced. Through analyzing the pseudo inverse, daisy-chain and quadratic programming allocation methods, control allocation modules of a flight control system were designed for an aircraft. Simulation resuits show the feature of each method and conclusions were presented at last.
作者 占正勇 刘林
出处 《飞行力学》 CSCD 北大核心 2006年第1期13-16,21,共5页 Flight Dynamics
关键词 多操纵面 控制分配 广义逆 二次规划 multi-control-effector control allocation generalized inverse, quadratic programming
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参考文献5

  • 1Kevin 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.
  • 2Reigelsperger W C,Banda S S.Nonlinear Simulation of a Modified F-16 with Full-Envelope Control Laws[J].Control Engineer Practice,1998,6 (2):309-320.
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