1 |
R. F. Jaggers, "An explicit solution to the exoatmospheric powered flight guidance and trajectory optimization problem for rocket propelled vehicles", AIAA 77-1051.
|
2 |
R. F. Jaggers, "Proposed powered explicit guidance thrust integrals derivation/ implementation", NASA CR-147796.
|
3 |
R. L. McHenry, T. J. Brand, A. D. Long, B. F. Cockrell, J. R. Thibodeau III, "Space shuttle ascent guidance, navigation, and control", J. Astronautical Sciences 27 (1), 1-38, 1979.
|
4 |
H. Nakagawa, Y. Ikeda, T. Mugitani, H. Suzuki, and H. Nakayasu, "An overview about guidance system for H-IIA Rocket", 제35회 비행기 심포지엄 강연집, pp. 125-128, 1997.
|
5 |
S. Ikeda and K. Tokita, "Development of H-II launch vehicle guidance software", Proc. of 5th ISCOPS, pp. 761-773, 1993.
|
6 |
송은정, 조상범, 박창수, 노웅래, "발사체 상단의 외연적 유도 알고리듬 적용 연구", 항공우주기술, 제 10권, 1호, pp.89-97, 2011.
|
7 |
D. C. Chandler and I. E. Smith, "Development of the iterative guidance mode with its application to various vehicles and missions", J. Spacecraft and Rockets, Vol. 4, No. 7, pp. 898-903, 1967.
DOI
|
8 |
mathworld.wolfram.com/IndefiniteIntegral
|
9 |
송은정, "H 유도 알고리듬 연구", KARI-LDT-TM-2011-011, 한국항공우주연구원, 2011.
|
10 |
M. Delporte and F. Sauvinet, "Explicit guidance law for manned spacecraft", AIAA 92-1145.
|