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- W2375457390 abstract "SST(satellite-satellite tracking) can provide size,shape and relative orientation of the classical constellation satellites,whereas it can not determine the absolute orientation of the constellation.To solve the problem of rank deficiency in SST autonomous orbit determination,spacecraft moving in Halo orbit,a kind of periodic orbits in CRTBP(circle restricted three body problem),is augmented into the classical constellation.The characteristic differences in force model between Halo orbit and perturbed Kepler orbit can remove the systematic correlation of state parameters of the traditional constellation,and thus prevent the overall constellation from rotating with respect to the inertial space.The mechanisms of force model and spatial configuration of Halo orbiters are analyzed.The multi-colinearity of the coefficient matrix of normal equation is investigated for the classical and libration orbit involved constellations.Some simulations using LMO-Halo crosslink range in CRTBP are designed to test the orbit determination method.The results show that owing to the involved libration orbit,autonomous orbit determination based on SST only,has the feasibility to estimate the absolute orientation of the constellation simultaneously." @default.
- W2375457390 created "2016-06-24" @default.
- W2375457390 creator A5052354691 @default.
- W2375457390 date "2013-01-01" @default.
- W2375457390 modified "2023-09-23" @default.
- W2375457390 title "SST Orbit Determination of Halo-LMO Constellation in CRTBP" @default.
- W2375457390 hasPublicationYear "2013" @default.
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