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Q-Law Aided Direct Trajectory Optimization of Many-Revolution Low-Thrust Transfers
- Source :
- Journal of Spacecraft and Rockets. 57:672-682
- Publication Year :
- 2020
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2020.
-
Abstract
- Low-thrust spacecraft trajectory optimization for the many-revolution orbital transfer problem is especially challenging due to the high problem dimension and perturbing accelerations that prevent ...
- Subjects :
- Propellant
Geostationary transfer orbit
Spacecraft
Computer science
business.industry
Aerospace Engineering
Thrust
Trajectory optimization
Nonlinear programming
Dimension (vector space)
Space and Planetary Science
Physics::Space Physics
Mathematics::Metric Geometry
Astrophysics::Earth and Planetary Astrophysics
Orbital maneuver
Aerospace engineering
business
Subjects
Details
- ISSN :
- 15336794 and 00224650
- Volume :
- 57
- Database :
- OpenAIRE
- Journal :
- Journal of Spacecraft and Rockets
- Accession number :
- edsair.doi...........a6f43b8a4b0f21885784ff9855554c4d