低推力推進式宇宙機による地球捕獲小惑星探査の軌道設計
| Project/Area Number |
15F15076
|
|---|
| Research Category |
Grant-in-Aid for JSPS Fellows
|
| Allocation Type | Single-year Grants |
|---|
| Section | 外国 |
|---|
| Research Field |
Aerospace engineering
|
|---|
| Research Institution | Japan Aerospace EXploration Agency |
|---|
Principal Investigator |
川勝 康弘 国立研究開発法人宇宙航空研究開発機構, 宇宙科学研究所, 准教授 (80373439)
|
|---|
| Co-Investigator(Kenkyū-buntansha) |
GARCIA YARNOZ DANIEL 国立研究開発法人宇宙航空研究開発機構, 宇宙科学研究所, 外国人特別研究員
|
|---|
| Project Period (FY) |
2015-10-09 – 2016-03-31
|
| Project Status |
Completed (Fiscal Year 2015)
|
| Budget Amount *help |
¥500,000 (Direct Cost: ¥500,000)
Fiscal Year 2015: ¥500,000 (Direct Cost: ¥500,000)
|
|---|
| Keywords | Lunar swing-bys / Tisserand-Pointcare / Sun pertubation / DESTINY / EQUULEUS |
|---|
| Outline of Annual Research Achievements |
Studied in this research is a systematic approach to generate first guesses of multiple lunar swing-by sequences for interplanetary small satellite missions. The Sun third body perturbation plays an important role essentially providing free v between lunar swing-bys. As a first approach, an extension of the classical Tisserand-Pointcar´e graph is presented, in which the potential gains by solar perturbation between flybys can be estimated. Secondly, following an approach proposed by Lantoine & McElrath, a database of Moon-to-Moon transfers is generated with a continuation method. New families with multiple revolutions and families close to libration point orbits are generated. The database can be accessed and transfers retrieved to quickly generate sequences in similar fashion to a Lambert problem solver. Two practical examples are presented: a transfer to the Earth-Moon L2 point, and an escape strategy for the DESTINY mission to initiate the transfer to asteroid Phaeton.
|
| Research Progress Status |
27年度が最終年度であるため、記入しない。
|
| Strategy for Future Research Activity |
27年度が最終年度であるため、記入しない。
|
Report
(1 results)
Research Products
(1 results)
