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Attitude & orbit control technique and optimal control in trajectory optimization at Thales Alenia Space
Thierry Dargent

Attitude & orbit control technique and optimal control in trajectory optimization at Thales Alenia Space

Author / Organization:
Science & Mathematics Published 2011 Verification Pending

Overview & Synopsis

In the last past years, low-thrust propulsion has evolved from a technological concept to a realistic option for interplanetary missions, it was considered first for very challenging trajectories to the inner planets, but now also for more classical ones, to Mars or the Moon. After Deep-Space 1, the first demonstration mission of the us of low-thrust propulsion for interplanetary missions and Smart 1 to the Moon, it becomes the baseline complex interplanetary mission In that context, Thales Alenia Space as increase its engineering capacity in interplanetary complex missions using chemical and/or low thrust propulsion

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Document Information

Document Title Attitude & orbit control technique and optimal control in trajectory optimization at Thales Alenia Space
Author / Organization Thierry Dargent
Subject & Discipline Multidisciplinary Academic Open Research
Categories Science & Mathematics
Publication Year 2011
License / Rights Open Access / Creative Commons
Resource Verification Listed PDF (Verification Pending)
Original Host Website HAL Open Science (hal.science)
File Format application/pdf (Portable Document Format)
Language EN
Catalog ID DOC-155723
Original Source Link Visit Source Page on hal.science »