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Differential Drag-Based Reference Trajectories for Spacecraft Relative Maneuvering Using Density Forecast

2016
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Journal of Spacecraft and Rockets
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A bc = element of matrix A d to which a Dcrit is the most sensitive A d = stable linear reference state-space matrix A s = Schweighart and Sedwick model state-space matrix a Dcrit = magnitude of the differential drag acceleration ensuring stability a Drel = magnitude of the differential aerodynamic drag acceleration a Prelx , a Prely = differential accelerations caused by orbital perturbations excluding drag, along x and y directions of the local vertical/local horizontal frame C DC , C DT =

doi:10.2514/1.a33332
fatcat:3qxzdiya2jflrdzt4mzxqwdat4