The system entry problem entails the capture of a spacecraft about a planet by way of propulsive maneuver(s) or flyby(s) of a planetary satellite(s), or both. In the case of the Jovian system, a balance is sought between the interplanetary time-of-flight, orbit insertion maneuver magnitude, mass delivered to the system, capture orbit period, radiation dose, and mission complexity. Based on a nominal asymptote, this paper introduces the analytical equations necessary to solve the phase-free, singly aided and doubly aided capture problems, with a focus on the doubly aided capture problem in the Jovian system. An analytical approximation for the required phasing is derived and the implications of the Laplace resonance are discussed. Analytical approximations are used to seamlessly seed a multiple-shooting algorithm in order to arrive at the converged high-fidelity solution space for the Europa Mission.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Dual Satellite-Aided Planetary Capture with Interplanetary Trajectory Constraints



    Published in:

    Publication date :

    2017




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    Local classification TIB:    770/7040
    BKL:    55.54 Flugführung



    Dual Satellite-Aided Planetary Capture with Interplanetary Trajectory Constraints

    Scott, Christopher J. / Ozimek, Martin T. / Haapala, Amanda F. et al. | AIAA | 2017



    Interplanetary Trajectories for Multiple Satellite-Aided Capture at Jupiter

    Lynam, Alfred E. / Longuski, James M. | AIAA | 2011