Comparison Study on Disturbance-compensated Intercept Guidance Using Line-of-sight Rate Information against Optimal Guidance
Author:
Affiliation:
1. Department of Aerospace Engineering, National Defense Academy of Japan
Publisher
The Society of Instrument and Control Engineers
Link
https://www.jstage.jst.go.jp/article/sicetr/55/3/55_216/_pdf
Reference18 articles.
1. 1) R.E. Machol, W.P. Tanner, Jr. and S.N. Alexander: System Engineering Handbook, Chap.19 Guidance, R.E. Hill (1965)
2. 3) Y. Yavin and R. De Villiers: Proportional Navigation and the Game of Two Cars: The Case of a Pursuer with Variable Speed, Computers Math with Applications, 18-1-3, 69/76 (1986)
3. 4) M.-J. Tahk, C.-S. Park and C.-K. Ryoo: Line-of-Sight Guidance Laws for Formation Flight, Journal of Guidance, Control, and Dynamics, 28-4, 708/716 (2005)
4. 5) Y. Sato, T. Yamasaki, H. Takano and Y. Baba: Trajectory Guidance and Control for a Small UAV, KSAS, 7-2, 137/144 (2006)
5. 6) M. Matsuda, H. Takano, T. Yamasaki and I. Yamaguchi: A Note on the Optimal Spacecraft Guidance, APISAT, 7.4.1.pdf (2012)
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