2019 Ninth International Conference on Intelligent Computing and Information Systems (ICICIS) 2019
DOI: 10.1109/icicis46948.2019.9014702
|View full text |Cite
|
Sign up to set email alerts
|

Spacecraft Orbital maneuver Flight Dynamics Simulation and Verification

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2021
2021
2021
2021

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(2 citation statements)
references
References 3 publications
0
2
0
Order By: Relevance
“…The coordinates u and θ are expressed as functions of using θ0 the equations of system (6), the left-hand sides of which have a simple form , and the right-hand sides depend not only on u and θ, but also on θ0. The variable is related to time t by (3). It remains to choose the first approximation by the Gilden choice in the same way as the Keplerian motion [10].…”
Section: Role Of Auxiliary Symbolsmentioning
confidence: 99%
See 1 more Smart Citation
“…The coordinates u and θ are expressed as functions of using θ0 the equations of system (6), the left-hand sides of which have a simple form , and the right-hand sides depend not only on u and θ, but also on θ0. The variable is related to time t by (3). It remains to choose the first approximation by the Gilden choice in the same way as the Keplerian motion [10].…”
Section: Role Of Auxiliary Symbolsmentioning
confidence: 99%
“…The motion of celestial bodies perpendicular to the plane of the Galaxy, obtaining the trajectory of motion, as well as studying them for stability can be used in Cosmonautics. In addition, the motion of celestial bodies in the perpendicular plane of the near-planetary disks and the equatorial plane of the Earth is very important for studying the mechanical characteristics of the motion of such celestial bodies as a comet, a meteorite [1]- [3].…”
Section: Introductionmentioning
confidence: 99%