Art

J-GLOBAL ID：201902282403170239   Reference number：19A2885452

Throttled Explicit Guidance for Future Pinpoint Landing Missions

将来の高精度着陸ミッションのための推力可変直接誘導

Author (3)： ITO TAKAHIRO (JAXA) ,  SAKAI SHIN'ICHIRO (JAXA) ,  UEDA SATOSHI (JAXA)
Material： 宇宙科学技術連合講演会講演集(CD-ROM)  (宇宙科学技術連合講演会(CD-ROM))
Volume： 63rd  Page： ROMBUNNO.1B09  Publication year： 2019 
JST Material Number： S0277B  ISSN： 1884-1945  Document type： Proceedings
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： space probe ,  *landing (alighting) ,  *control ,  *optimum control ,  *thrust control ,  vector control ,  mass ,  specific thrust ,  switching ,  orbit (trajectory) ,  simulation ,  predictor-corrector method ,  variable of state ,  load ,  computation workload ,  lunar surface ,  flying object
Semi thesaurus term： *Selenological and Engineering Explorer-2 ,  thrust vector control ,  fuel consumption ,  *induction control ,  asteroid probe

JST classification (4)： Motion and orbit of space crafts  (QK02060W) ,  Flight control systems  (QK05020Z) ,  Operating technology  (QK05030K) ,  Space crafts  (QK08000Y)

Reference (8)：

• A. R. Klumpp, “Apollo Lunar Descent Guidance,” Automatica, Vol. 10, pp. 133-146, 1974.
• R. L. McHenry, T. J. Brand, A. D. Long, et al., “Space Shuttle Ascent Guidance, Navigation, and Control,” The Journal of the Astronautical Sciences, Vol. 27, No. 1, pp. 1-38, 1979.
• D. Dueri, A. B. Acikmese, B. Scharf, and M. W. Harris, “Customized Real Time Int erior Point Methods for Onboard Powered Descent Guidance,” Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, pp. 197-212, 2017.
• P. Lu, “Propellant Optimal Powered Descent Guidance,” Journal of Guidance, Control, and Dynamics, Vol. 41, No. 4, pp. 813-826, 2018.
• T. Ito and S. Sakai, “ Throttled Explicit Guidance for Planetary and Pinpoint Landing,” 70th International Astronautical Congress, IAC-19-C1.7.7, 2019

Terms in the title (5)： 着陸 ,  ミッション ,  推力 ,  可変 ,  誘導