Robust-Backstepping Missile Autopilot Design Considering Time-Varying Parameters and Uncertainty

Lee Seokwon; Kim Youdan; Lee Yongwoo; Moon Gwanyoung; Jeon Byung-Eul

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Robust-Backstepping Missile Autopilot Design Considering Time-Varying Parameters and Uncertainty

机译：考虑时变参数和不确定性，强大的反伸位导弹自动驾驶仪设计

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Missile autopilots for aerodynamic angle control and acceleration control are designed for fin-controlled missiles during the boost phase. In the boost phase, the speed change and the parameter variation of the missile are fast and large. To deal with the time-varying characteristics of the missile, the time-varying parameters are considered in nonlinear dynamics, and the parametric uncertainties are modeled. A state-feedback controller is designed for aerodynamic angle control based on a robust-backstepping scheme. Also, an output feedback controller is designed for acceleration control, where the acceleration dynamics are derived using input-output linearization. Numerical simulations are performed to demonstrate the performance of the proposed controllers.

机译：用于空气动力角度控制和加速度控制的导弹自动驾驶仪专为在升压阶段进行翅片控制导弹而设计。在升压阶段，导弹的速度变化和参数变化是快速且大的。为了处理导弹的时变特征，在非线性动力学中考虑时变参数，并且参数化不确定度被建模。基于鲁棒备份方案的空气动力角度控制设计了一种状态反馈控制器。此外，输出反馈控制器设计用于加速控制，其中使用输入输出线性化导出加速动态。执行数值模拟以证明所提出的控制器的性能。

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来源
《IEEE Transactions on Aerospace and Electronic Systems》 |2020年第6期|4269-4287|共19页
作者
Lee Seokwon; Kim Youdan; Lee Yongwoo; Moon Gwanyoung; Jeon Byung-Eul;
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作者单位

Seoul Natl Univ Inst Adv Aerosp Technol Dept Aerosp Engn Seoul 08826 South Korea;

Seoul Natl Univ Inst Adv Aerosp Technol Dept Aerosp Engn Seoul 08826 South Korea;

Agcy Def Dev Daejeon 34186 South Korea;

Agcy Def Dev Daejeon 34186 South Korea;

Agcy Def Dev Daejeon 34186 South Korea;

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正文语种 eng
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关键词
Missiles; Aerodynamics; Uncertainty; Acceleration; Nonlinear dynamical systems; Backstepping; Boost phase; missile autopilot; robust backstepping; uncertainty model;

机译：导弹;空气动力学;不确定性;加速度;非线性动力系统;BackStepping;升压阶段;导弹自动驾驶仪;强大的BackStepping;不确定性模型;

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专利

1. Robust H_∞ autopilot design for agile missile with time-varying parameters [J] . Mahmood A., Kim Y., Park J. Aerospace and Electronic Systems, IEEE Transactions on . 2014,第4期

机译：具有时变参数的敏捷导弹的鲁棒H _{∞自动驾驶仪设计}
2. Roll-pitch-yaw autopilot design for nonlinear time-varying missile using partial state observer based global fast terminal sliding mode control [J] . Ahmed Awad, Wang Haoping 中国航空学报（英文版） . 2016,第005期

机译：基于局部状态观测器的全局快速终端滑模控制的非线性时变导弹横滚偏航自动驾驶仪设计
3. Adaptive sliding mode autopilot design for skid-to-turn missile model with uncertainties [J] . Ra Chunggil, Kim Seungkeun, Suk Jinyoung International Journal of Control, Automation, and Systems . 2017,第6期

机译：自适应滑模自动驾驶仪设计，具有不确定性的滑动到转动导弹模型
4. Adaptive Backstepping Autopilot Design for Missiles of Fast Time-varying Velocity [C] . Seokwon Lee, Youdan Kim, Guanyoung Moon, IFAC Symposium on Automatic Control in Aerospace . 2016

机译：快速时变速器导弹自适应Backstepping自动驾驶仪设计
5. Adaptive control of linear time-varying systems with applications to missile autopilots. [D] . Song, Chanho. 1989

机译：线性时变系统的自适应控制及其在导弹自动驾驶仪上的应用。
6. Synchronization criteria of discrete-time complex networks with time-varying delays and parameter uncertainties [O] . P. Balasubramaniam, L. Jarina Banu 2014

机译：具有时变时滞和参数不确定性的离散时间复杂网络的同步准则
7. Roll-pitch-yaw autopilot design for nonlinear time-varying missile using partial state observer based global fast terminal sliding mode control [O] . Awad Ahmed, Wang Haoping 2016

机译：基于局部状态观测器的全局快速终端滑模控制的非线性时变导弹横滚偏航自动驾驶仪设计

Robust-Backstepping Missile Autopilot Design Considering Time-Varying Parameters and Uncertainty

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