Attitude Controller Design and Test of Korea Space Launch Vehicle-I Upper Stage
Author:
Publisher
The Korean Society for Aeronautical & Space Sciences
Link
http://ocean.kisti.re.kr/downfile/crosscheck/ksass/JAKO201007049675374.pdf
Cited by 3 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. A Numerical Study on the Effect of the Umbilical Plate on Longitudinal Controllability of a Low Aspect Ratio Launch Vehicle;International Journal of Aeronautical and Space Sciences;2019-07-17
2. Longitudinal Aerodynamic Coefficients Estimation and Identifiability Analysis for Hypersonic Glider Controlled by Moving Mass;International Journal of Aeronautical and Space Sciences;2019-01-02
3. Quaternion-based attitude control design and hardware-in-the-loop simulation of suborbital modules with cold gas thrusters;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-06-20
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