## Collection of Technical Papers |

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### Contents

Spacecraft LOUIS KINGSLAND JR and WILLARD E BOLLMAN | |

DONALD J JEZEWSKI and JUDITH M STOOLZ | |

INDEX | |

3 other sections not shown

### Common terms and phrases

accuracy adjoint AIAA analysis analytical angle angular momentum approximately argument of periapsis argument of pericenter Astrodynamics Astronautics asymptote axis boundary conditions branched trajectory canonical transformation coefficients components constant convergence damping defined deployment derived determined differential equations Earth eccentric orbits eccentricity effects elliptic equa equations of motion error evaluated expansions flight flyby Galilean moons given gradient gravitational gravity-gradient Halley's Comet Hamiltonian hodograph hyperbolic impulsive initial conditions injection iteration Jupiter Lagrange multiplier Libration linear low-thrust magnitude maneuver mass matrix minimum-fuel mission O-locus oblateness obtained optimal optimum orbit plane orbital period parameters parking orbit periapsis perigee perturbations problem radial radius right ascension rocket rotational satellite second order second thrusting interval semimajor axis shown in Figure solution spacecraft stability stopover orbit swingby technique terminal tion torque trajec transfer trajectory true anomaly variables velocity increment velocity vector zero