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pro vyhledávání: '"Sinha, Amlan"'
Spacecraft trajectory design is a global search problem, where previous work has revealed specific solution structures that can be captured with data-driven methods. This paper explores two global search problems in the circular restricted three-body
Externí odkaz:
http://arxiv.org/abs/2410.02976
Autor:
Sinha, Amlan, Beeson, Ryne
The growing interest in the cislunar domain over the past decade has led to an increasing demand for low-thrust missions to key orbits within this region. These low-thrust missions, typically characterized by long thrust arcs, are highly susceptible
Externí odkaz:
http://arxiv.org/abs/2410.00297
Autor:
Sinha, Amlan, Beeson, Ryne
As low-thrust space missions increase in prevalence, it is becoming increasingly important to design robust trajectories against unforeseen thruster outages or missed thrust events. Accounting for such events is particularly important in multibody sy
Externí odkaz:
http://arxiv.org/abs/2409.19905
Preliminary trajectory design is a global search problem that seeks multiple qualitatively different solutions to a trajectory optimization problem. Due to its high dimensionality and non-convexity, and the frequent adjustment of problem parameters,
Externí odkaz:
http://arxiv.org/abs/2308.03960
Publikováno v:
Proceedings of SPIE; 6/25/2017, Vol. 10400, p104001U-1-104001U-13, 13p
Optimization of high-inclination orbits using planetary flybys for a zodiacal light-imaging mission.
Publikováno v:
Proceedings of SPIE; 6/25/2017, Vol. 10400, p104001X-1-104001X-13, 13p
Publikováno v:
Proceedings of SPIE; September 2017, Vol. 10400 Issue: 1 p104001X-104001X-13, 10296113p
Autor:
Shaklan, Stuart, Soto, Gabriel, Sinha, Amlan, Savransky, Dmitry, Delacroix, Christian, Garrett, Daniel
Publikováno v:
Proceedings of SPIE; September 2017, Vol. 10400 Issue: 1 p104001U-104001U-13, 10296113p