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Volume 33 Issue 06
Jun.  2007
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Journal of Beijing University of Aeronautics and Astronautics  > 2007  >  33(06): 709-713.
Yang Lingyu, Guo liang, Liu Jiarun, et al. Design and simulation of integrated flight and propulsion control for post stall maneuvers[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(06): 709-713. (in Chinese)
Citation: Yang Lingyu, Guo liang, Liu Jiarun, et al. Design and simulation of integrated flight and propulsion control for post stall maneuvers[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(06): 709-713. (in Chinese)
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Design and simulation of integrated flight and propulsion control for post stall maneuvers

  • School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 14 Jul 2006
  • Publish Date: 30 Jun 2007
    Abstract
  • Research on simulation and design of IFPC(integrated flight and propulsion control system ) of super angle of attack maneuver were done for an advanced vectored-thrust aircraft. A new structure of IFPC was put forward. An engine stability control system was designed to enhance engine stability at super angle. Moment requirements were calculated by rigid body inverse dynamic method, and the aerodynamic surfaces and thrust vector were allocated by the optimal control allocation and the saturation principle. Simulation results show that engine operates steadily, and thrust vector supplies extra moment, when the aerodynamic surfaces moment is not enough. The dynamic response of system is rapid, and tracking characteristic is well.

     

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  • [1] 王立峰,张津.超机动飞行推进系统稳定性控制研究[J]. 推进技术,2000,21(4):1-4 Wang Lifeng,Zhang Jin.Propulsion system stability control for super-maneuvering flight[J]. Journal of Propulsion Technology, 2000,21(4):1-4 (in Chinese) [2] 叶茂林,申功璋. 带推力矢量综合飞行推进控制系统设计及其仿真研究 .北京:北京航空航天大学自动化科学与电器工程学院,2002 Ye Maolin,Shen Gongzhang.Design and simulation research for integrated flight/propulsion system .Beijing:School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,2002(in Chinese) [3] Delaat J C,Southwick R D,Gallops G W.High stability engine control .AIAA-96-2586,1996 [4] 柳嘉润,申功璋. 基于逆动力学和在线参数辨识的飞机姿态控制[J]. 北京航空航天大学学报,2005,31(2):111-115 Liu Jiarun,Shen Gongzhang.Attitude control based on inverse dynamics and online parameter identification[J].Journal of Beijing University of Aeronautics and Astronautics, 2005,31(2):111-115 (in Chinese) [5] Yang Lingyu,Shen Gongzhang.A new optimal control allocation method for aircraft with multiple control effectors .AIAA-2007-1052,2007
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