Targeting Applying ε-Bounded Orbit Correction Perturbations
1998 ◽
Vol 08
(07)
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pp. 1575-1584
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Keyword(s):
A low-sized chaotic trajectory is used to compute epsilon-bounded orbit correction perturbations in order to rapidly target a trajectory from the vicinity of a starting point to a target. An algorithm that allows fast computation of a set of perturbations to be applied is presented, and its performance is tested in a higher-dimensional system, the kicked double rotor.
2019 ◽
Vol 475
(2222)
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pp. 20180504
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Keyword(s):
2018 ◽
Vol 474
(2209)
◽
pp. 20170612
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2000 ◽
2020 ◽
Vol 17
(6)
◽
pp. 2684-2688
2016 ◽
Vol 14
(06)
◽
pp. 1640028
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Keyword(s):
2016 ◽
Vol 30
(3)
◽
pp. 413-430
◽
Keyword(s):
Keyword(s):
2006 ◽
Vol 39
(13)
◽
pp. 3283-3293
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