| Citation: | SUN Y Q，QIANG H R，DONG K H，et al. Derivation and application of iterative scheme for angle-only orbit determination[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3245-3252 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0062
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Regarding the problem of the angle-only orbit determination, we transformed into a method for solving the minimum value of the fitness function. The difference and relationship between the observation time step, the dynamic equation solution step and the iterative format step are analyzed. It is pointed out that the difficulty of precise orbit determination mainly lies in the high nonlinearity of the fitness function. A new method combining the initial and precise orbit determination is thus proposed, and its feasibility is analyzed theoretically. Finally, the accuracy, effectiveness and efficiency of the proposed method are verified by numerical experiments.
| [1] |
BENNETT J C, SANG J, SMITH C, et al. An analysis of very short-arc orbit determination for low-Earth objects using sparse optical and laser tracking data[J]. Advances in Space Research, 2015, 55(2): 617-629. doi: 10.1016/j.asr.2014.10.020
|
| [2] |
LI B, SANG J, CHEN J. Achievable orbit determination and prediction accuracy using short-arc space-based observations of space debris[J]. Advances in Space Research, 2018, 62(11): 3065-3077. doi: 10.1016/j.asr.2018.08.038
|
| [3] |
GAIAS G, ARDAENS J S. Flight demonstration of autonomous noncooperative rendezvous in low Earth orbit[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(6): 1337-1354. doi: 10.2514/1.G003239
|
| [4] |
GONG B, LI W, LI S, et al. Angles-only initial relative orbit determination algorithm for non-cooperative spacecraft proximity operations[J]. Astrodynamics, 2018, 2(3): 217-231. doi: 10.1007/s42064-018-0022-0
|
| [5] |
MILANI A, GRONCHI G F, KNEZEVIC Z, et al. Orbit determination with very short arcs[J]. ICARUS, 2005, 179(2): 350-374. doi: 10.1016/j.icarus.2005.07.004
|
| [6] |
VALLADO D A, CARTER S S. Accurate orbit determination from short-arc dense observational data[J]. Journal of the Astronautical Sciences, 1998, 46(2): 704-729.
|
| [7] |
贾沛璋, 吴连大. 论初轨计算的最佳精度及二重解[J]. 天文学报, 1998, 39(4): 337-343. doi: 10.15940/j.cnki.0001-5245.1998.04.001
JIA P Z, WU L D. The optimal accuracy and double solution of initial orbit calculation are discussed[J]. Acta Astronomica Sinica, 1998, 39(4): 337-343(in Chinese). doi: 10.15940/j.cnki.0001-5245.1998.04.001
|
| [8] |
ANSALONE L, CURTI F. A genetic algorithm for Initial orbit determination from a too short arc optical observation[J]. Advances in Space Research, 2013, 52(3): 477-489. doi: 10.1016/j.asr.2013.04.004
|
| [9] |
HINAGAWA H, YAMAOKA H, HANADA T. Orbit determination by genetic algorithm and application to GEO observation[J]. Advances in Space Research, 2014, 53(3): 532-542. doi: 10.1016/j.asr.2013.11.051
|
| [10] |
LI X R, WANG X. Genetic algorithm for initial orbit determination with too short arc[J]. Acta Astronomica Sinica, 2016, 41(1): 76-91.
|
| [11] |
LI X R, WANG X. Genetic algorithm for initial orbit determination with too short arc (continued)[J]. Chinese Astronomy and Astrophysics, 2017, 41(2): 254-262. doi: 10.1016/j.chinastron.2017.04.007
|
| [12] |
LI X R, WANG X, XIONG Y Q. A combination method using evolutionary algorithms in initial orbit determination for too short arc[J]. Advances in Space Research, 2019, 63(2): 999-1006. doi: 10.1016/j.asr.2018.08.036
|
| [13] |
王雪莹, 安玮, 李骏. 天基光学短弧观测约束域的粒子群优化定轨方法[J]. 国防科技大学学报, 2014, 36(6): 146-151. doi: 10.11887/j.cn.201406026
WANG X Y, AN W, LI J. An orbit-determination method with particle swarm optimization using space-based optical short-arc observation in admissible region[J]. Journal of National University of Defense Technology, 2014, 36(6): 146-151(in Chinese). doi: 10.11887/j.cn.201406026
|
| [14] |
周海银, 潘晓刚, 李董辉. 基于天基空间目标监视系统的定轨技术研究[J]. 系统仿真学报, 2008, 20(13): 3538-3541. doi: 10.16182/j.cnki.joss.2008.13.065
ZHOU H Y, PAN X G, LI D H. Research on orbit determination algorithm based on SBSS[J]. Journal of System Simulation, 2008, 20(13): 3538-3541(in Chinese). doi: 10.16182/j.cnki.joss.2008.13.065
|
| [15] |
杨志涛. 低地球轨道初轨确定误差分析[J]. 空间碎片研究, 2019, 19(2): 1-9.
YANG Z T. Eroor analysis of initial orbit determination in low Earth orbit[J]. Space Debris Research, 2019, 19(2): 1-9(in Chinese).
|
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