BR

B. Riha

2 records found

Feature Engineering for Low-Thrust Trajectory Optimization

A Systematic Analysis Using Pontryagin Fuel-Optimal Earth-Mars Transfer Trajectories

Using low-thrust propulsion for interplanetary space missions has the potential to allow for more payload for the same mass put into orbit compared to what impulsive propulsion would allow for. The disadvantages are found in mission planning, however, as the continuous nature of ...
This is the final report in a project which aims to design a mega-constellation to survey the Earth for environmental, safety and security reasons: monitoring gases, humans, vehicles, and potential other aspects such as forest fires...