Aerodynamic Surfaces Control Allocation for RLV Reentry

摘要：

In this paper, aerodynamic control surfaces of reusable launch vehicle (RLV) in reentry phase were converted into a constrained optimization problem, and using a mixed linear programming algorithm to solve them. For nonlinear between aerodynamic control surfaces and control torque, the piecewise linear programming algorithm was used to solve the control surfaces failure and on-line reconflgurable optimization problem. Finally, simulation verify three failure modes of aerodynamic surfaces by piecewise linear programming method and aerodynamic surfaces can be reconstructed with good performance and a smaller allocation error.

关键词： reusable launch vehicle control allocation aerodynamic control surfaces mixed integer linear programming

作者: XU Zhi TANG Shuo

作者单位: College of Astronautics Northwestern Polytecnical University Xian,China

会议类型: 国际会议

会议名称: 2010 Second International Conference on Intelligent Human-Machine Systems and Cybernetics(第二届智能人机系统与控制论国际学术会议 IHMSC 2010)

会议地点: 南京

会议语种:英文

页码: 73-76

在线出版日期: 2010-08-26（万方平台首次上网日期，不代表论文的发表时间）