Determination Technology and Accuracy Analysis of Configuration Parameters of Ground System Dual Satellite Formation Based on Navigation Data

Author:

Kai Du,Haiyue Li,Jiangpeng Liang,Yanrong Wang,Dan Wang,Jing Cao,Shilu Shen

Publisher

Springer Nature Singapore

Reference7 articles.

1. Hall, C.E., Shtessel, Y.B.: Sliding mode disturbance observer-based control for a reusable launch vehicle. J. Guidance Control Dynamics 29(6), 1315–1328 (2006)

2. Simone, D.A., Ardaens, J.S., Larsson, R.: GNSS-based space borne autonomous formation flying experiment (SAFE) on PRISMA: Initial Commissioning - AIAA/AAS Astrodynamics Specialist Conference (2010)

3. Shao, K., et al.: Analysis of tiangong-2 orbit determination and prediction using onboard dual-frequency GNSS data. GPS Solutions 24(1), 1–13 (2019)

4. Kai, S.H.A.O., et al.: Precise absolute and relative orbit determination for distributed InSAR satellite system. Acta Geodaetica et Cartographica Sinica 50(5), 580 (2021)

5. Du, Y., Yang, G., Wang, W.: E/I vector design method for InSAR satellite formation configuration. Shanghai Aerospace 28(5), 6(2011):

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