发明名称 |
METHOD FOR AUTONOMOUS NAVIGATION AND ORIENTATION OF SPACECRAFT BASED ON VIRTUAL MEASUREMENTS OF ZENITH DISTANCES OF STARS |
摘要 |
FIELD: physics. ^ SUBSTANCE: position of spacecraft in three-dimensional space, the unitary radius-vector and other elements of the reference (calculated, a priori assumed) orbit of the spacecraft are determined based on use of information coming from optoelectron devices mounted on the body of the spacecraft. The minimum number of required optoelectron devices is three, and two of them are placed in gimbals for optimum viewing of selected brightest stars of the celestial sphere. One optoelectron device is rigidly connected to the body of the spacecraft and measures coordinates and brightness of stars falling in the field of vision during navigation sessions and identifies the brightest (working) star. ^ EFFECT: broader functional capabilities. ^ 2 dwg |
申请公布号 |
RU2454631(C1) |
申请公布日期 |
2012.06.27 |
申请号 |
RU20100144278 |
申请日期 |
2010.10.28 |
申请人 |
GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA VOENNO-KOSMICHESKAJA AKADEMIJA IMENI A.F. MOZHAJSKOGO |
发明人 |
KUZNETSOV VLADISLAV IVANOVICH;DANILOVA TAMARA VALENTINOVNA;KOSULIN DMITRIJ MIKHAJLOVICH |
分类号 |
G01C21/02 |
主分类号 |
G01C21/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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