Linear correction of a maneuver trajectory by means of impulses

Details Linear correction of a maneuver trajectory by means of impulses Linear correction of a maneuver trajectory by means of impulses

Jul 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978kosis..16..619l&link_type=abstract

Kosmicheskie Issledovaniia, vol. 16, July-Aug. 1978, p. 619-621. In Russian.

Physics

Fuel Consumption, Spacecraft Maneuvers, Specific Impulse, Thrust Programming, Trajectory Control, Burning Rate, Fuel Tanks, Propulsive Efficiency, Trajectory Optimization

Scientific paper

A solution to the minimum fuel consumption problem of using multiple
impulses to control a trajectory involving numerous maneuvers is
presented. The solution is obtained under the assumption that the fuel
consumed for correction and maneuvers is stored in the same tank.

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