Optimal acceleration of spacecraft with electroreactive engine for bounded rate of rotation of thrust vector

Details Optimal acceleration of spacecraft with electroreactive engine for bounded rate of rotation of thrust vector Optimal acceleration of spacecraft with electroreactive engine for bounded rate of rotation of thrust vector

Nov 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976cosre..14..305v&link_type=associated

(Kosmicheskie Issledovaniia, vol. 14, May-June 1976, p. 336-342.) Cosmic Research, vol. 14, no. 3, Nov. 1976, p. 305-310. Trans

Computer Science

Numerical Analysis

Electric Rocket Engines, Low Thrust Propulsion, Optimal Control, Spacecraft Trajectories, Trajectory Optimization, Angular Velocity, Boundary Value Problems, Computer Techniques, Differential Equations, Equations Of Motion, Gravitational Effects, Hamiltonian Functions, Numerical Analysis, Pontryagin Principle, Variational Principles

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