Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry | |
Li WH(李文皓); Xiao XX(肖歆昕); Zhang H(张珩); Xiao XX(肖歆昕) | |
会议录名称 | 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 |
2017 | |
会议名称 | 21st AIAA International Space Planes and Hypersonics Technologies Conference |
会议日期 | 6-9 March 2017 |
会议地点 | Xiamen, China |
摘要 | In this paper, a new angle-of-attack(AOA) guidance law and controller with multi-control surface and reaction control system (RCS) are designed to reduce normal acceleration in sub-orbit re-entry phase. First, the six-degree-of-freedom (6-DOF) nonlinear dynamic model of sub-orbit vehicles established, and the overload characteristics is analyzed under traditional AOA guidance law. Second, an AOA guidance law added height element is proposed to reduce the Normal accelerate peak value during re-entry. Furthermore, an Inverse-PIDA control law and composite control strategy are designed to control multi-aerodynamic surface and RCS. Finally the proposed approach is applied in a sub-orbit vehicle re-entry flight, validation simulation are conducted by using the proposed guidance law and controller with the 6-DOF nonlinear dynamic model , Monte-Carlo statistical analysis shows it can get well control performance with 卤20% aerodynamic elements uncertainty and random wind. 漏 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. |
关键词 | Aerodynamics Air Navigation Angle Of Attack Control Surfaces Control Theory Degrees Of Freedom (Mechanics) Dynamic Models Flight Control Systems Flight Simulators Monte Carlo Methods Reentry Spacecraft Surface Reactions Uncertainty Analysis Vehicles |
ISBN号 | 978-1-62410-463-3 |
URL | 查看原文 |
收录类别 | EI |
语种 | 英语 |
文献类型 | 会议论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/72198 |
专题 | 先进制造工艺力学实验室 |
通讯作者 | Xiao XX(肖歆昕) |
推荐引用方式 GB/T 7714 | Li WH,Xiao XX,Zhang H,et al. Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry[C]21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,2017. |
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