| タイトル | Numerical Roll Reversal Predictor Corrector Aerocapture and Precision Landing Guidance Algorithms for the Mars Surveyor Program 2001 Missions |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040090584 |
| 著者（英） | Powell, Richard W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1998-01-01 |
| 言語 | eng |
| 内容記述 | This paper describes the development and evaluation of a numerical roll reversal predictor-corrector guidance algorithm for the atmospheric flight portion of the Mars Surveyor Program 2001 Orbiter and Lander missions. The Lander mission utilizes direct entry and has a demanding requirement to deploy its parachute within 10 km of the target deployment point. The Orbiter mission utilizes aerocapture to achieve a precise captured orbit with a single atmospheric pass. Detailed descriptions of these predictor-corrector algorithms are given. Also, results of three and six degree-of-freedom Monte Carlo simulations which include navigation, aerodynamics, mass properties and atmospheric density uncertainties are presented. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | AIAA Paper 98-4574 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/88388 |
