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Trajectory optimization and guidance for a Hermes-type reentry vehicle
The paper presents a guidance scheme and several optimal reentry trajectories for a HERMES type reentry vehicle from a low-earth orbit mission to a landing site in Southern France. The guidanceExpand
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  • 1
Multi-Phase Trajectory Optimization Methods with Applications to Hypersonic Vehicles
Numerical solutions of multi-phase optimal control problems are considered, where a phase is defined as a subinterval in which the right-hand sides of the differential equations are continuous. Expand
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