Abstract
In this paper, we present the application of the ZEM/ZEV guidance algorithm to the planar restricted three-body problem (PR3BP). The ZEM/ZEV guidance law as a feedback guidance strategy is presented and applied to the PR3BP. The fuel optimal solution to the PR3BP for a transfer from GTO to L<inf>1</inf> in the Earth-Moon system is presented as a point for comparison, showing the near optimality of the closed-loop guidance approach. Challenges of the approach and strategies for implementation in spacecraft mission design are discussed.
| Original language | English (US) |
|---|---|
| Title of host publication | Advances in the Astronautical Sciences |
| Publisher | Univelt Inc. |
| Pages | 575-584 |
| Number of pages | 10 |
| Volume | 152 |
| ISBN (Print) | 9780877036111 |
| State | Published - 2014 |
| Event | 24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States Duration: Jan 26 2014 → Jan 30 2014 |
Other
| Other | 24th AAS/AIAA Space Flight Mechanics Meeting, 2014 |
|---|---|
| Country/Territory | United States |
| City | Mexico |
| Period | 1/26/14 → 1/30/14 |
ASJC Scopus subject areas
- Aerospace Engineering
- Space and Planetary Science