This project forked from hirsar/spacecraft-trajopt-reorientation
Optimal spacecraft reorientation due to momentum exchange using point internal masses in 2D
Optimal spacecraft reorientation due to momentum exchange using point internal masses in 2D
Using CasADi's NLP interface and the IPOPT optimizer, I solved optimal trajectories for min time and min energy objectives for circular, square, rectangular, and bowtie spacecraft shapes. Trapezoidal time discretization was applied.
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