講題:Computational Optimal Control Techniques and Their Applications in Space Missions
時間:10/03(二)下午 13:30
地點:綜合三館837室
摘要:The optimal control is a commonly-used technique with a broad range of applications in aerospace engineering, such as the spacecraft/launcher optimal design problems. For instance, during the mission design stage, one of the main tasks is to find an optimal trajectory of the rocket to maximize the mass of a payload or to minimize the duration of the flight from launch to satellite insertion subject to the physical constraints and the insertion conditions. One other example is an inter-planetary probe traveling between two orbits. During the mission operation stage, aerospace engineers need to design an optimal trajectory to reduce the consumption of fuel to extend its mission life further. In this talk, we provide a comprehensive survey of state-of-the-art solution algorithms for trajectory optimization problems. Some current collaboration with engineers at National Space Organization, Taiwan, and Taiwan Innovative Space, Inc. is also introduced.
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