Evaluation of Optical Magnitude of Deep Space Spacecraft

Simple item page
dc.creatorWei, Liu
dc.creatorZheng-Hong, Tang
dc.creatorYong-Da, Li
dc.date2007-12-10
dc.date.accessioned2026-07-07T08:48:21Z
dc.date.available2026-07-07T08:48:21Z
dc.descriptionOptical-electric technology can measure the tangential position and velocity of spacecraft. To know the feasibility of the use of optical-electric technology, it is necessary to estimate the magnitude of spacecraft first. Since the spacecrafts are non-self-illumination objects, the estimation formulas of the optical magnitude of spacecraft is constructed according to the radiation theory and the extra-atmospheric radiant emittance of the Sun in the visible light wave band. Taking Chang'e-1 as an example, the magnitude of it in different situations is calculated.
dc.descriptionPublished in Proceedings of the 14th Young Scientists Conference on Astronomy and Space Physics, Kyiv, Ukraine, April 23-28, 2007
dc.identifierhttps://arxiv.org/abs/0712.1552
dc.identifierhttp://arxiv.org/abs/0712.1552
dc.identifierYSC'14 Proceedings of Contributed Papers (eds. G. Ivashchenko, A. Golovin), Kyiv, Kyivskyi Universytet, pp. 82-86, 2007
dc.identifier.urihttp://salesiana.dossiersoluciones.com/handle/123456789/143915
dc.subjectAstrophysics
dc.titleEvaluation of Optical Magnitude of Deep Space Spacecraft
dc.typetext

Files

Collections

arXiv