참고문헌
- Isakowitz, S. J., Hopkins, J. P. Jr., and Hopkins, J. B., International Reference Guide to Space Launch Systems, 3rd Ed., AIAA, 1999.
- Greensite, A. L., Analysis and Design of Space Vehicle Flight Control Systems, Spartan Books, New York, 1970.
- McHenry, R. L., Brand, T.J., Long, A. D., Cockrell, B. F., and Thibodeau, J. R, "Space Shuttle Ascent Guidance, Navigation, and Control," The Journal of the Astronautical Sciences, vol. XXVII, no. 1, pp. 1-38, 1979.
- 노웅래 외 5인, "중형과학로켓의 자세제어기 설계," 98 한국자동제어학술회의 논문집, pp. 1099-1102, 1998. 10.
- 노웅래 외 8인, "KSR-III 로켓의 스트랩다운 관성항법시스템 개발," 한국항공우주학회 2001년도 추계학술발표회,pp. 956-959, 2001.11.
- Anon., Effects of Structural Flexibility on Launch Vehicle Control Systems, NASA SP-8036, Feb, 1970.
- Morita Y, and Kawaguchi, J., "Approaches to Control Design of Flexible Structures," 5th Workshop on Astrodynamics and Flight Mechanics, pp. 82-87, Aug., 1995.
- Hill, A.D., An Investigation of the Flight Vibrations Experienced during the METEOR Mission of the Conestoga Launch Vehicle, M.S. Thesis of the University of Alabama, 1996.
- Slivinsky, S.H., Galloway, R.G., Bukley, A.P., "Missile Technology Demonstration Flight Test-2 : Lessons Learned," 21st Annual AAS Rocky Mountain Guidance and Control Conference, pp. 613-632, Feb., 1998.
- Frosch, J. A. and Vallely, D. P., "Saturn AS501/S-IC Flight Control System Design," Journal of Spacecraft and Rocket, vol. 4, no. 8, pp. 1003-1009, Aug., 1967. https://doi.org/10.2514/3.29009
- 노웅래 외 6인, "KSR-III 로켓의 휨모드 안정화 필터 설계," 제3회 우주발사체기술 심포지움, pp.163-170, 2002.3.
- 안재명 외 3인, "시간지연을 갖는 추력기 자세제어시스템의 Limit Cycle 분석, KACC 2000, TAD01-3, 2000.10.
- 조현철,노웅래,안재명, "KSR-III 로켓의 벤딩필터 구현과 비행후 스펙트럴 분석," 제4회 우주발사체기술 심포지움, pp. 266-274, 2003.5.