Impact Angle Control Guidance of Glide-Capable Munition Using a Vector Field Approach-Reference-Cited by-同舟云学术

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Impact Angle Control Guidance of Glide-Capable Munition Using a Vector Field Approach

Published:2021-04 Issue:2 Volume:57 Page:1069-1083
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Lee Suwon,Kim Youdan,Song Chanho

Funder

LIG Nex1

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/9399890/09257069.pdf?arnumber=9257069

Cited by 10 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. An Optimization Method of Attitude Control Parameters Based on Genetic Algorithm for the Boost-Glide Rocket;IEEE Transactions on Aerospace and Electronic Systems;2024-08

2. Path Modification Algorithm for Collision Avoidance Using Offset Curves of Pythagorean Hodograph Curves;Journal of the Korean Society for Aeronautical & Space Sciences;2023-08-31

3. Quaternion-based 3D Attitude Tracking Algorithm Using Virtual Roll Angle for Missile Systems;International Journal of Control, Automation and Systems;2023-08-25

4. Hardware-in-the-Loop Simulation Test Method for the Inertial Navigation System of a Boost-Glide Rocket;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18

5. Impact Speed Control Guidance for Glider Vehicle Using Optimal Output Trajectory Shaping Algorithm;Journal of the Korean Society for Aeronautical & Space Sciences;2023-03-31

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