| タイトル | The Mars Surveyor 2001 Lander: A First Step Toward Precision Landing |
| 著者（英） | Braun, Robert D.; Mase, Robert A.; Spencer, David A.; Cheatwood, F. McNeil; Powell, Richard W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1998-01-01
1998 |
| 言語 | eng |
| 内容記述 | As the robotic exploration of Mars continues, science objectives have driven mission and flight system development towards the use of precision landing technology such that small surface features, such as craters, can be investigated. In addition, the surface rendezvous elements of human exploration missions will require landing accuracy that is greatly improved over that achievable with ballistic flight. With improved approach navigation and hypersonic maneuvering technologies, the MSP'01 Lander is taking the first significant step toward precision landing on Mars. This advance requires both the ability to generate lift during the atmospheric flight and an on-board guidance algorithm to direct a three-axis control system. Many configuration options were examined to generate the required lift, with an afterbody-mounted deployable flap emerging as the lightest-weight solution. Five candidate guidance algorithms have been developed and submitted to the MSP'01 Project for evaluation. Through high-fidelity simulation, each of these algorithms has demonstrated the ability to greatly improve upon the landed accuracy provided by ballistic flight. As a result, the science community should expect to be within 10 km of the specified landing target. In fact, depending on the selected aeroshell L/D, a 5-km precision landing goal is achievable with greater than 90% confidence. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | IAF-98-Q.3.03 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/344561 |
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