This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.
JPL, Voyager Mission. http://voyager.jpl.nasa.gov/JPLVoyager Mission.http://voyager.jpl.nasa.gov/Search in Google Scholar
NASA, Cassini, Solstice Mission. http://cassini-2.jpl.nasa.gov/NASA, CassiniSolstice Mission.http://cassini-2.jpl.nasa.gov/Search in Google Scholar
JPL, Galileo Mission. http://Galileo.jpl.nasa.gov/JPLGalileo Mission.http://Galileo.jpl.nasa.gov/Search in Google Scholar
Wilson R. S. and Howell K. C. Trajectory Design in the Sun Earth Moon System Using Lunar Gravity Assists. Journal of Spacecraft and Rockets. (35): 191–198 (1998). 10.25/2.3309WilsonR. S.HowellK. C.Trajectory Design in the Sun Earth Moon System Using Lunar Gravity AssistsJournal of Spacecraft and Rockets.35191198199810.25/2.3309Open DOISearch in Google Scholar
Curtis H. D. Orbital Mechanics for Engineering Students. (2005) http://Elsevier.com/CurtisH. D.Orbital Mechanics for Engineering Students.2005http://Elsevier.com/Search in Google Scholar
Marchand B. G., Howell K. C., and Wilson R. S. Improved Corrections Process for Constrained Trajectory Design in the n-Body Problem. Journal of Spacecraft and Rockets. (44): 884 – 897 (2007). 10.2514/1.27205MarchandB. G.HowellK. C.WilsonR. S.Improved Corrections Process for Constrained Trajectory Design in the n-Body ProblemJournal of Spacecraft and Rockets.44884897200710.2514/1.27205Open DOISearch in Google Scholar
Vasile M., Bernelli-Zazzera F., Jehn R., Janin G. Optimal Interplanetary Trajectories Using a Combination of Low- Thrust and Gravity Assist Manoeuvres. Rio de Janeiro, Brazil, IAF-00-A.5.07, 51st IAF Congress (2000).VasileM.Bernelli-ZazzeraF.JehnR.JaninG.Optimal Interplanetary Trajectories Using a Combination of Low- Thrust and Gravity Assist Manoeuvres.Rio de JaneiroBrazilIAF-00-A.5.07, 51st IAF Congress2000Search in Google Scholar
Betts J. T. Optimal Interplanetary Orbit Transfers by Direct Transcription. The Journal of the Astronautical Sciences. (40): 247–268 (1994).BettsJ. T.Optimal Interplanetary Orbit Transfers by Direct TranscriptionThe Journal of the Astronautical Sciences.402472681994Search in Google Scholar
Vasile M. Direct Transcription by FET for Optimal Space Trajectory Design. Internal Report DIASR 99–02, Politecnico di Milano, Dipartimento di Ingegneria Aerospaziale (1999).VasileM.Direct Transcription by FET for Optimal Space Trajectory DesignInternal Report DIASR9902Politecnico di MilanoDipartimento di Ingegneria Aerospaziale1999Search in Google Scholar
Bate R. R., Mueller D. D. and White J. E. Fundamentals of Astrodynamics. Dover Publications, Mineola (1971).BateR. R.MuellerD. D.WhiteJ. E.Fundamentals of Astrodynamics.Dover PublicationsMineola1971Search in Google Scholar