Matches in SemOpenAlex for { <https://semopenalex.org/work/W2067431831> ?p ?o ?g. }
Showing items 1 to 82 of
82
with 100 items per page.
- W2067431831 endingPage "295" @default.
- W2067431831 startingPage "288" @default.
- W2067431831 abstract "The short-arc orbit determination to be discussed here means a method of initial orbit calculation without a priori information that bypasses multi-variate iteration. It requires that the concerned dynamical problem has an approximate analytical solution, which can represent the short arc to a certain degree of accuracy. When the lunar probe enters the effective range of lunar gravitational force and approaches the moon, the dynamical problem can be treated as a perturbed 2-body problem relative to the moon, and when the probe is close to the earth, then as a perturbed 2-body problem relative to the earth, but for the whole transition stage, it can only be treated as a perturbed restricted 3-body problem. The restricted 3-body problem has no analytical solution, even when outside the effective range of lunar gravitation and for the large-thrust impulsive transfer, the eccentricity of the varying elliptical orbit relative to the earth is so large (greater than the Laplace limit) that an analytical solution can not be constructed. When the lunar gravitational perturbation is taken into consideration, we have constructed a time power series solution for the segment of transfer orbit that takes into consideration the coaction of a nonspherical earth (including only the J2-term) and the moon, and on this basis, a method for initial orbit calculation in the sense of perturbed 2-body problem. Numerical verification of this method indicates that it is effective as a short-arc orbit determination and that it will be useful to the ground-based measurement and control systems." @default.
- W2067431831 created "2016-06-24" @default.
- W2067431831 creator A5025111951 @default.
- W2067431831 creator A5053538039 @default.
- W2067431831 date "2007-07-01" @default.
- W2067431831 modified "2023-09-23" @default.
- W2067431831 title "A Method of Short-arc Orbit Determination for the Transfer Orbit of Lunar Probes" @default.
- W2067431831 cites W1968018775 @default.
- W2067431831 doi "https://doi.org/10.1016/j.chinastron.2007.06.003" @default.
- W2067431831 hasPublicationYear "2007" @default.
- W2067431831 type Work @default.
- W2067431831 sameAs 2067431831 @default.
- W2067431831 citedByCount "2" @default.
- W2067431831 countsByYear W20674318312023 @default.
- W2067431831 crossrefType "journal-article" @default.
- W2067431831 hasAuthorship W2067431831A5025111951 @default.
- W2067431831 hasAuthorship W2067431831A5053538039 @default.
- W2067431831 hasConcept C107768556 @default.
- W2067431831 hasConcept C110605091 @default.
- W2067431831 hasConcept C121332964 @default.
- W2067431831 hasConcept C124017977 @default.
- W2067431831 hasConcept C125311221 @default.
- W2067431831 hasConcept C127413603 @default.
- W2067431831 hasConcept C1276947 @default.
- W2067431831 hasConcept C146978453 @default.
- W2067431831 hasConcept C147843779 @default.
- W2067431831 hasConcept C173990265 @default.
- W2067431831 hasConcept C17744445 @default.
- W2067431831 hasConcept C177918212 @default.
- W2067431831 hasConcept C190538878 @default.
- W2067431831 hasConcept C19269812 @default.
- W2067431831 hasConcept C196644772 @default.
- W2067431831 hasConcept C199539241 @default.
- W2067431831 hasConcept C29829512 @default.
- W2067431831 hasConcept C34725247 @default.
- W2067431831 hasConcept C51244244 @default.
- W2067431831 hasConcept C71427050 @default.
- W2067431831 hasConcept C74650414 @default.
- W2067431831 hasConcept C94042562 @default.
- W2067431831 hasConceptScore W2067431831C107768556 @default.
- W2067431831 hasConceptScore W2067431831C110605091 @default.
- W2067431831 hasConceptScore W2067431831C121332964 @default.
- W2067431831 hasConceptScore W2067431831C124017977 @default.
- W2067431831 hasConceptScore W2067431831C125311221 @default.
- W2067431831 hasConceptScore W2067431831C127413603 @default.
- W2067431831 hasConceptScore W2067431831C1276947 @default.
- W2067431831 hasConceptScore W2067431831C146978453 @default.
- W2067431831 hasConceptScore W2067431831C147843779 @default.
- W2067431831 hasConceptScore W2067431831C173990265 @default.
- W2067431831 hasConceptScore W2067431831C17744445 @default.
- W2067431831 hasConceptScore W2067431831C177918212 @default.
- W2067431831 hasConceptScore W2067431831C190538878 @default.
- W2067431831 hasConceptScore W2067431831C19269812 @default.
- W2067431831 hasConceptScore W2067431831C196644772 @default.
- W2067431831 hasConceptScore W2067431831C199539241 @default.
- W2067431831 hasConceptScore W2067431831C29829512 @default.
- W2067431831 hasConceptScore W2067431831C34725247 @default.
- W2067431831 hasConceptScore W2067431831C51244244 @default.
- W2067431831 hasConceptScore W2067431831C71427050 @default.
- W2067431831 hasConceptScore W2067431831C74650414 @default.
- W2067431831 hasConceptScore W2067431831C94042562 @default.
- W2067431831 hasIssue "3" @default.
- W2067431831 hasLocation W20674318311 @default.
- W2067431831 hasOpenAccess W2067431831 @default.
- W2067431831 hasPrimaryLocation W20674318311 @default.
- W2067431831 hasRelatedWork W1044062963 @default.
- W2067431831 hasRelatedWork W1516258657 @default.
- W2067431831 hasRelatedWork W1592631157 @default.
- W2067431831 hasRelatedWork W1661182353 @default.
- W2067431831 hasRelatedWork W190906238 @default.
- W2067431831 hasRelatedWork W2052204230 @default.
- W2067431831 hasRelatedWork W2067431831 @default.
- W2067431831 hasRelatedWork W2360222860 @default.
- W2067431831 hasRelatedWork W2886819650 @default.
- W2067431831 hasRelatedWork W2995132996 @default.
- W2067431831 hasVolume "31" @default.
- W2067431831 isParatext "false" @default.
- W2067431831 isRetracted "false" @default.
- W2067431831 magId "2067431831" @default.
- W2067431831 workType "article" @default.