Bank-to-Turn Guidance Law with Terminal Impact-Angle Constraint

Author:

Qiuqiu Wen1,Qunli Xia2,Weixia Su3

Affiliation:

1. Lecturer, Dept. of Aerospace, Beijing Institute of Technology, Zhongguanchun South St., Beijing 100081, P.R.China (corresponding author).

2. Assistant Professor, Dept. of Aerospace, Beijing Institute of Technology, Zhongguanchun South St., Beijing 100081, P.R.China.

3. Senior Research Engineer, Beijing Institute of Mechanical Equipment, Yongding St., Beijing 100039, P.R.China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference17 articles.

1. Aggrawal R. K. and Moore C. R. (1984). “A bank-to-turn guidance law.” GACIAC PR 85–01 GACIAC IIT Research Center Chicago.

2. Terminal Guidance Algorithm for Ramjet-Powered Missiles

3. Status and concerns for bank-to-turn control of tactical missiles

4. Advances in missile guidance theory;Ben-Asher J. Z.;Prog. Astronaut. Aeronaut.,1998

5. Nonlinear Autopilot Design for an Asymmetric Missile Using Robust Backstepping Control

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Impact-angle-constrained reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-07-10

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