1 |
B. Wie, H. Weiss and A. Araposiathis, "Quaternion Feedback Regulator for Spacecrft Eigenaxis Rotations," Jounal of Guidence, vol12, No.3, May-June, 1989, pp. 375-377.
DOI
ScienceOn
|
2 |
이승우, 최홍택, 김진철, “다목적 실용위성 태양모드 및 기동모드의 추력기 제어 설계,” 한국항공우주학회지, 제27권, 제2호, 1999년, pp. 82-89.
|
3 |
방효충, 탁민제, 김진형, “추력기를 이용한 유연 우주비행체의 자세제어,” 한국항공우주학회지, 제29권, 제4호, 2001년, pp. 93-100.
|
4 |
Jahn, Robert J. Jahn, Physics of Electric Propulsion, McGraw-Hill, New York, 1968.
|
5 |
James R. Wertz, Spacecraft Attitude Determintion and Control, D. Reidel Publishing Company, Holland, 1978.
|
6 |
James R. Wertz and Wiley J. Larson, Space Mission Anlalysis and design, Space Technology Library, Boston, 1991.
|
7 |
박영웅, 방효충, 박태호, “무궁화위성 1,2호의 추력기 자세제어 연구: 11-Timer 방식과 Tone-Pulse 방식,” 한국항공우주학회지, 제27권, 제6호, 1999년, pp. 73-79.
|
8 |
Guman, W. J. and David, M. N., "Pulsed Plasma Microthruster Propulsion System for Synchronous Orbit Satellite," Journal of Spacecraft and Rockets, Vol. 7, No.4, April, 1970, pp. 409-415.
DOI
|
9 |
Loh, W. H. T., Jet, Rocket, Nuclear, Ion and electirc Propulsion, Springer-Verlag, New York, 1968.
|
10 |
Marshall H. Kaplan, Modern Spacecraft Dynamics & Control, John Willey & Sons, New York, 1976.
|
11 |
Guman, W. J. and Peko, P. E., "Solid-Propellant Pulsed Plasma Microthruster," Journal of Spacecraft and Rockets, Vol. 5, No.6, June, 1968, pp. 732-733.
DOI
|
12 |
99년도 인공위성연구센터 기관고유사업보고서, 인공위성센터, 1999.
|
13 |
Jungyoup Han, Youngwoong Park, "Fuzzy Controller Design for Attitude control of Spacecraft with a Flexible Appendage," Proc. of the 14th Korea Automatic Control Conference, Yongin, Korea, 1999, pp.C69-C72.
|