References
- 장영근, "국내외 소형위성 연구 개발 동향과 전망", 한국항공우주학회 추계학술발표회 논문집, 2002.
- Alok Das and Richard Cobb "TechSat 21 - Space Missions Using Collaborating Constellation of Satellites", 12th AIAA/USU Conference of Small Satellites, 1998.
- http://www.vs.afrl.af.mil/TechProgs/TechSat21/
- http://sim.jpl.nasa.gov/michelson/iss2002/lay.htm
- http://sim.jpl.nasa.gov/michelson/iss2002/lay.pdf
- http://sci.esa.int/content/doc/b3/26803_.htm #P10_2623
- John Adams, et al,. "Technologies for Spacecraft Formation Flying" supported under NASA contract, Stanford University, 1996.
- http://nmp.jpl.nasa.gov/st3/edu
- http://planetquest.jpl.nasa.gov/TPF/ tpf_index.html
- http://sci.int/home/lisa/index.cfm
- http://maxim.gsfc.nasa.gov/
- http://space.gsfc.nasa.gov/astro/specs/
- http://nasa.asu.edu/ASUSat/3CS/
- http://ssdl-delta.stanford.edu/Emerald
- http://www.aa.washington.edu/research /dawgstar/overview.html
- Jeffrey G. Reichbach, et al., "Micropropulsion System Selection for Precision Formation Flying Satellites" January 30, 2001 at MIT.
- Hill, G. W., "Researches in the Lunar Theory", American Journal of Mathematics, Vol. 1, No. 1, 1878, pp. 5-26. https://doi.org/10.2307/2369430
- Gokhan Inalhan, et al., "Relative dynamics and control of spacecraft formations in eccentric orbits", Journal of Guidance, Control and Dynamics, Vol. 25, No. 1, 2002, pp. 48-59. https://doi.org/10.2514/2.4874
- Koji Yamanaka, et al., "New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit", Journal of Guidance, Control and Dynamics, Vol. 25, No. 1, 2002, pp. 60-66. https://doi.org/10.2514/2.4875
- William E. Wiesel, "Relative Satellite Motion About an Oblate Planet", Journal of Guidance, Control and Dynamics, Vol. 25, No. 4, 2002, pp. 776-785. https://doi.org/10.2514/2.4946
- Samuel A. Schweighart, "High-Fidelity Linearized J2 Model for Satellite Formation Flight", Journal of Guidance, Control and Dynamics, Vol. 25, No. 6, 2002, pp. 1073-1080. https://doi.org/10.2514/2.4986
- Wang Sang Koon, et al., "J2 Dynamics and Formation Flight", AIAA paper No. 2001-4090, 2001.
- Dong-Woo Gim, et al., "The State Transition Matrix of Relative Motion for the Perturbed Non-circular Reference Orbit", AAS 01-222, 2001.
- Hanspeter Schaub, et al., "J2 Invariant Relative Orbits for Spacecraft Formations", Celestial Mechanics and Dynamical Astronomy, 79: 2001, pp. 77-95. https://doi.org/10.1023/A:1011161811472
- David F. Chichka, "Satellite Clusters with Constant Apparent Distribution", Journal of Guidance, Control and Dynamics, Vol. 24, No. 1, 2001, pp. 117-122. https://doi.org/10.2514/2.4683
- Kyle T. Alfriend, et al., "Gravitational Perturbations, Nonlinearity and Circular Orbit Assumption Effects on Formation Flying Control Strategies", AAS 00-012, 2000.
- 유성문 외, "위성 편대비행을 위한 궤도 설계와 수치적 방법을 이용한 동역학 모델의 검증", 한국항공우주학회 춘계학술발표회 논문집, 2003.
- P. K. C. Wang, et al., "Minimum-Fuel Formation Reconfiguration of Multiple Free-Flying Spacecraft", Journal of the Astronautical Sciences, Vol. 47, No. 1, 1999, pp. 77-102.
- Randal W. Beard, et al., "Fuel Optimization for Constrained Rotation of Spacecraft Formations", Journal of Guidance, Control and Dynamics, Vol. 23, No. 2, 2000, pp. 339-346. " https://doi.org/10.2514/2.4528
- Randal W. Beard, et al., "Fuel Equalized Retargeting for Separated Spacecraft lnterferometry", American Control Conference, Philadelphia, PA, June, 1998, pp. 1580-1584.
- Randal W. Beard, et al., "Fuel Optimization for Unconstrained Rotation of Spacecraft Formations", Journal of the Astronautical Sciences, vol. 43, no. 3, 1999, pp. 259-273
- Edmund Mun-Choong Kong, "Spacecraft Formation Flight Exploiting Potential Fields", Ph.D Thesis, Department of Aeronautics and Astronautics, MIT, 2002.
- P. K. C. Wang, et al., "Synchronized Formation Rotation and Attitude Control of Multiple Free-Flying Spacecraft", Journal of Guidance, Control and Dynamics, Vol. 22, No. 1, 1999, pp. 28-35. https://doi.org/10.2514/2.4367
- Jonathan R. Lawton, "Synchronized Multiple Spacecraft Rotations", Automatica, Vol. 38, No. 8, 2002, pp. 1359-1364. https://doi.org/10.1016/S0005-1098(02)00025-0
- Richards, A. et al., "Plume Avoidance Maneuver Planning Using Mixed Integer Linear Programming", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2001-4091, 2001.
- Gcikhan Inalhan, et al., "Precise Formation Flying Control of Multiple Spacecraft Using Carrier-phase Differential GPS" AAS 00-109, 2000.
- Luis M. Gomes. "FFDEM: Demonstration Formation Flying with Small Spacecraft" 16th Annual/USU Conference on Small Satellite, 2002.
- http://www.colorado.edu/geography/gcraf t/notes/gps/gps.html#PPS
- Chan-Woo Park, "Precise Relative Navigation Using Augmented CDGPS", Ph.D Thesis, Department of Mechanical engineering, Stanford Univ., 2001.
Cited by
- The establishment of requirement and kinematic analysis of mechanism for deployable optical structure vol.42, pp.8, 2014, https://doi.org/10.5139/JKSAS.2014.42.8.701