Adaptive Spacecraft Attitude Control and Asteroid Parameter Estimation
Author:
Publisher
Springer Nature Switzerland
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-40579-2_24
Reference19 articles.
1. Guelman, M.: Closed-loop control of close orbits around asteroids. J. Guidance Control Dyn. 38(5), 854–860 (2015). https://doi.org/10.2514/1.G000158
2. Furfaro, R., Cersosimo, D., Wibben, D.: Asteroid precision landing via multiple sliding surfaces guidance techniques. J. Guidance Control Dyn. 36(4), 1075–1092 (2013). https://doi.org/10.2514/1.58246
3. Gui, H., Ruiter, A.H.J.: Control of asteroid-hovering spacecraft with disturbance rejection using position-only measurements. J. Guidance Control Dyn. 40(10), 2401–2416 (2017). https://doi.org/10.2514/1.G002617
4. Lee, K.W., Singh, S.N.: Adaptive and supertwisting adaptive spacecraft orbit control around asteroids. J. Aerosp. Eng. 32(4) (2019). https://doi.org/10.1061/(ASCE)AS.1943-5525.0001043
5. Misra, A.K., Panchenko, Y.: Attitude dynamics of satellites orbiting an asteroid. J. Astronaut. Sci. 54, 369–381 (2006). https://doi.org/10.1007/BF03256495
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