有限时间误差收敛轨迹生成,带视场和角度约束

Q3 Earth and Planetary Sciences
Ye Chen, Shufan Wu, Xiaoliang Wang, Di Zhang, Jun Jia, Quan Li
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引用次数: 0

摘要

本文提出了一种结合终端角度约束和寻的器视场限制的归航制导法则,用于打击静止目标。所提出的制导方案由比例导航制导和与新定义的角度误差有关的连续反馈项组成。考虑到许多现有方法都使用开关逻辑策略来解决会产生不连续加速指令的特定约束,而本文提出的方案不使用开关逻辑,从而克服了这一限制。此外,通过类似 Lyapunov 的方法保证了截获前角度误差的有限时间收敛,还设计了一个整形函数来延长误差为零的范围。数值模拟证明了所提出的制导法则的特点和优势。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Finite-time error convergent trajectory generation with field-of-view and angle constraints

Finite-time error convergent trajectory generation with field-of-view and angle constraints

A homing guidance law combined with terminal angle constraint and seeker’s field-of-view limit is proposed in this paper for hitting a stationary target. The proposed guidance scheme is composed of proportional navigation guidance and a continuous feedback term with respect to a newly defined angle error. Considering that many existing methods use switching logic strategy to address the specific constraint which will generate discontinuous acceleration command, the proposed scheme overcomes the limitation by not using switching logic. Furthermore, the finite-time convergence of angle error before interception is guaranteed via a Lyapunov-like approach, a shaping function is also designed to lengthen the range at which the error becomes zero. Numerical simulations demonstrate the characteristics and advantages of the proposed guidance law.

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来源期刊
Aerospace Systems
Aerospace Systems Social Sciences-Social Sciences (miscellaneous)
CiteScore
1.80
自引率
0.00%
发文量
53
期刊介绍: Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion
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