Start solution for interplanetary low thrust trajectory optimization and model refinement. Volume 3: Low thrust orbit optimization for interplanetary missions using a Pontryagin/Lambert approach
Abstract
Descriptions are given of the package written for the European Space Operations center for low thrust orbit control problem solving.
- Publication:
-
Start solution for interplanetary low thrust trajectory optimization and model refinement. Volume 3: Low thrust orbit optimization for interplanetary missions using a Pontryagin/Lambert approach ESA
- Pub Date:
- March 1985
- Bibcode:
- 1985ssil....3.....H
- Keywords:
-
- Interplanetary Trajectories;
- Low Thrust;
- Pontryagin Principle;
- Trajectory Optimization;
- User Manuals (Computer Programs);
- Asteroid Missions;
- Fortran;
- Orbital Mechanics;
- Satellite Orbits;
- Astrodynamics