Analysis of Petal Rotation Trajectory Characteristics

[1]  J. C. Smith,et al.  Design of the Cassini tour trajectory in the Saturnian system , 1995 .

[2]  Nathan J. Strange,et al.  Cycler Trajectories in Planetary Moon Systems , 2009 .

[3]  Shane D. Ross,et al.  Resonance and Capture of Jupiter Comets , 2001 .

[4]  C. Murray,et al.  Solar System Dynamics: Expansion of the Disturbing Function , 1999 .

[5]  Kathleen C. Howell,et al.  Three-Dimensional Periodic Halo Orbits , 1981 .

[6]  Rodney L. Anderson,et al.  Role of Invariant Manifolds in Low-Thrust Trajectory Design , 2004 .

[7]  Ryan P. Russell,et al.  Endgame Problem Part 1: V-Infinity-Leveraging Technique and the Leveraging Graph , 2010 .

[8]  Fernando Peralta,et al.  Cassini Interplanetary Trajectory Design , 1995 .

[9]  L. D. Friedman,et al.  Orbit design concepts for Jupiter orbiter missions , 1974 .

[10]  Spatial p-q Resonant Orbits of the RTBP , 2002 .

[11]  Victor Szebehely,et al.  Chapter 10 – Modifications of the Restricted Problem , 1967 .

[12]  Roby S. Wilson,et al.  Improved Corrections Process for Constrained Trajectory Design in the n-Body Problem , 2007 .

[13]  Rodney L. Anderson,et al.  A Dynamical Systems Analysis of Resonant Flybys: Ballistic Case , 2011 .

[14]  Rodney L. Anderson,et al.  Dynamical Systems Analysis of Planetary Flybys and Approach: Planar Europa Orbiter , 2010 .

[15]  Nathan J. Strange,et al.  A fast tour design method using non-tangent v-infinity leveraging transfer , 2010 .

[16]  Ryan P. Russell,et al.  Flybys in the planar, circular, restricted, three-body problem , 2012 .

[17]  Brent Buffington,et al.  Jovian Tour Design for Orbiter and Lander Missions to Europa , 2014 .