Low-thrust Lambert transfer based on two-stage constant-vector thrust control method
Low-thrust Lambert transfer based on two-stage constant-vector thrust control method
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Publisher
Dordrecht: Springer Netherlands
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Language
English
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Publisher
Dordrecht: Springer Netherlands
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Scope and Contents
Contents
The low-thrust Lambert transfer refers to that the spacecraft achieves the orbital transfer whose boundary conditions are represented by two sets of orbital elements at initial and final time by the low-thrust propulsion system. The modulus and direction of the low-thrust solutions in previous methods change with time, which leads to high control r...
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Full title
Low-thrust Lambert transfer based on two-stage constant-vector thrust control method
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Record Identifier
TN_cdi_proquest_journals_2708604287
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_proquest_journals_2708604287
Other Identifiers
ISSN
0924-090X
E-ISSN
1573-269X
DOI
10.1007/s11071-022-07608-y
