Full text
|
PDF
- Requires a PDF viewer, such as GSview, Xpdf or Adobe Acrobat Reader
Download (1MB) | Preview |
Optimal 3D orbit corrections in curvilinear coordinates
Citation
Gonzalo Gomez, Juan Luis and Bombardelli, Claudio (2016). Optimal 3D orbit corrections in curvilinear coordinates. In: "26th AAS/AIAA Space Flight Mechanics Meeting", 14-18 feb, Napa, California (EEUU). ISBN 978-0-87703-633-3. pp. 397-414.
Description
| Title: | Optimal 3D orbit corrections in curvilinear coordinates |
|---|---|
| Author/s: |
|
| Item Type: | Presentation at Congress or Conference (Article) |
| Event Title: | 26th AAS/AIAA Space Flight Mechanics Meeting |
| Event Dates: | 14-18 feb |
| Event Location: | Napa, California (EEUU) |
| Title of Book: | Advances in the Astronautical Science : Spaceflight Mechanics 2016 |
| Date: | 2016 |
| ISBN: | 978-0-87703-633-3 |
| Volume: | 158 |
| Subjects: | |
| Faculty: | E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM) |
| Department: | Física Aplicada a las Ingenierías Aeronáutica y Naval |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
The minimum-time, constant-thrust orbit correction between two close non-coplanar circular orbits is studied using a relative motion formulation in curvilinear coordinates. The associated optimal control problem in the thrust orientation is tackled using the direct method to numerically solve a diverse set of problems for varying orbital radius and inclination. Additionally, an analytical estimate for the minimum-time inclination change maneuver is obtained. Fundamental changes in the structure of the solution and objective function are highlighted depending on the relation between the required radial displacement, inclination change and available thrust.
Funding Projects
| Type | Code | Acronym | Leader | Title |
|---|---|---|---|---|
| Government of Spain | ESP2013-41634-P | Unspecified | Unspecified | Análisis dinámico, propagación orbital avanzada y simulación de sistemas espaciales complejos |
| Government of Spain | FPU13/05910 | Unspecified | Unspecified | Unspecified |
| FP7 | 607457 | LEOSWEEP | Sener | Improving Low Earth Orbit Security With Enhanced Electric Propulsion |
More information
| Item ID: | 46659 |
|---|---|
| DC Identifier: | https://oa.upm.es/46659/ |
| OAI Identifier: | oai:oa.upm.es:46659 |
| Official URL: | http://www.univelt.com/linkedfiles/v158%20Contents.pdf |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 25 Feb 2019 09:16 |
| Last Modified: | 04 Sep 2020 14:47 |
