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Multi-objective hybrid optimal control for interplanetary mission planning (Document No: 20150010093)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Englander, Jacob |
| Copyright Year | 2015 |
| Description | Preliminary design of low-thrust interplanetary missions is a highly complex process. The mission designer must choose discrete parameters such as the number of flybys, the bodies at which those flybys are performed, and in some cases the final destination. Because low-thrust trajectory design is tightly coupled with systems design, power and propulsion characteristics must be chosen as well. In addition, a time-history of control variables must be chosen which defines the trajectory. There are often many thousands, if not millions, of possible trajectories to be evaluated. The customer who commissions a trajectory design is not usually interested in a point solution, but rather the exploration of the trade space of trajectories between several different objective functions. This can be very expensive process in terms of the number of human analyst hours required. An automated approach is therefore very desirable. This work presents such an approach by posing the mission design problem as a multi-objective hybrid optimal control problem. The methods is demonstrated on hypothetical mission to the main asteroid belt and to Deimos. |
| File Size | 1304872 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20150010093 |
| Archival Resource Key | ark:/13960/t8z947p5k |
| Language | English |
| Publisher Date | 2015-04-01 |
| Access Restriction | Open |
| Subject Keyword | Trajectory Design Optimization Low Thrust Asteroid Belts Systems Engineering Optimal Control Propulsion Mission Planning Trajectories Space Exploration Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |