Analytical approximate solution of the problem of a spacecraft’s optimal turn with arbitrary boundary conditions
Work
Year: 2015
Type: article
Authors А. В. Молоденков, Ya. G. Sapunkov
Institution Institute of Precision Mechanics and Control
Cites: 7
Cited by: 16
Related to: 10
FWCI: 1.073
Citation percentile (by year/subfield): 87.36
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed