Abstract
For solving the weak observability problem of angle-only relative state estimate, a multi-spacecraft collaborative observation method is proposed. The multi-spacecraft collaboration angle-only relative state estimate model is developed, including state equation and measurement equation. Firstly, based on the second-order relative motion equation, the system state equation is established; secondly, considering the line-of-sight angle measured by different spacecrafts, the system measurement equation is established; then the unscented Kalman filter algorithm is used to estimate the target’s relative state. Finally, the numerical simulation validates that the aforementioned method can effectively improve the weak observability of angle-only relative state estimate, and with the increasing of the number of spacecrafts, the convergence speed and accuracy of the relative position, velocity are also higher. In addition, the performance of the aforementioned method under uncertainty is also validated by two scenarios where the measurement data is sometimes lost and the target is maneuvered.
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References
Qi, L., Sun, L.C., Gong, Z.Z., et al.: Micro space debris detection technology and applications. Space Debris Res. 21(2), 10–16 (2021)
Ardaens, J.S., Gaias, G.: Angles-only relative orbit determination in low earth orbit. Adv. Space Res. 61(11), 2740–2760 (2018)
Pi, J., Bang, H.: Trajectory design for improving observability of angles-only relative navigation between two spacecrafts. J. Astronautical Sci. 61(4), 391–412 (2014)
Zhang, Y.Z., Huang, P.F.: An angle-only navigation ang control scheme for noncooperative rendezvous operations. IEEE Trans. Industr. Electron. 66(11), 8618–8627 (2019)
Gong, B.C., Wang, S., Hao, M.R., et al.: Cooperative relative navigation algorithm for multi-spacecraft close-range formation. J. Astronautics 42(03), 344–350 (2021)
Zhao, K.: State estimation algorithms under non-ideal condition and its application in angle-only relative navigation, pp. 115–124. Harbin Institute of Technology, Haerbin (2021)
Gaias, G., D’amico, S., Ardaens, J.S.: Angles-only navigation to a noncooperative spacecraft using relative orbital elements. J. Guid. Control. Dyn. 37(2), 439–451 (2014)
Han, F., Liang, Y., Guo, W.T., et al.: A method of relative navigation using line-of-sight angles on spacecraft: ZL 201110011003.1[P]. 2015–7–15
Yuan, M.: Relative navigation methods of flying formation in large ellipitical orbit based on angles-only information, pp. 46–55. Harbin Institute of Technology, Haerbin (2017)
Han, F., Liu, F.C., Wang, Z.L., et al.: Multiple line-of-sight angles-only relative navigation by multiple collaborative space robots. Acta Aeronautica et Astronautica 42(1), 316–326 (2021)
Gao, X.H., Liang, B., Pan, L.: High-orbit non-cooperative target multi-line of sight distributed relative navigation method. J. Astronautics 36(3), 292–299 (2015)
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© 2023 Bei**g HIWING Sci. and Tech. Info Inst
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Dawei, F., Weiwei, C., Le**, Y., Runde, Z. (2023). Relative State Estimate of Non-cooperative Target by Multiple Spacecraft Collaborative Observation. In: Fu, W., Gu, M., Niu, Y. (eds) Proceedings of 2022 International Conference on Autonomous Unmanned Systems (ICAUS 2022). ICAUS 2022. Lecture Notes in Electrical Engineering, vol 1010. Springer, Singapore. https://doi.org/10.1007/978-981-99-0479-2_197
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DOI: https://doi.org/10.1007/978-981-99-0479-2_197
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Publisher Name: Springer, Singapore
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Online ISBN: 978-981-99-0479-2
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