Examples for research results generation

[ChristopherRabotin]

To simplify the generation of figures for my thesis, a command should be able to do the following:

• [x] Starting from an initial orbit at a given time, perform correction using the two control laws available
• [x] Orbit must be generated in both directions
• [x] Must include all test cases from the Naasz, Ruggerio and Petropoulos papers for simple comparison
• [ ] Should also plot fuel usage
• [x] Show examples about Mars (ExoMars TGO insert to final orbit maybe?)

/!\ Run these on threads with different files names so I can run them overnight on GCE.

[ChristopherRabotin]

Hum, so I implemented those as tests and did that directly on master. Bad practice, but it works.

[ChristopherRabotin]

Plots or tables:

• [ ] Thrust level versus T.O.F. in days and fuel usage starting at an inclined GTO and at an MRO. Show similar to Earth to Mars and Mars to Earth (consider the best case scenario of the v_infinity). Min thrust should be that of Dawn, max is a VX-200 (must determine thrust step, maybe based on integer increment of thrusters).
• [x] Relative V_infinity at Earth and Mars (use data generated on GCP): goes in the chapter for the selection of the parking orbit at Earth.
• [ ] Example scenario of optimal correction from the initial GTO injection, to a GTO with an arbitrary inclination different from GTO (e.g. a 1 degree difference). Tug then performs several maneuvers to reach GTO again at different dates (suppose a two days gaps between launches to reconfigure Air Force tracking and ranging antennas).
• [ ] Example scenario around Mars using parking orbits of active probes (e.g. for a deployment of both ExoMars, MRO).
• [ ] Plot the alpha and beta angles of the thrusting direction for the example scenarios.
• [ ] Repeat the three previous scenarios with different thrust levels.

[ChristopherRabotin]

Done in #101 (and by sending thesis to committee).