High-precision shape approximation low-thrust trajectory optimization method satisfying bi-objective index
نویسندگان
چکیده
منابع مشابه
Low-Thrust, High-Accuracy Trajectory Optimization
Multirevolution, very low-thrust trajectory optimization problems have long been considered difficult problems due to their large time scales and high-frequency responses. By relating this difficulty to the well-known problem of aliasing in information theory, an antialiasing trajectory optimization method is developed. The method is based on Bellman’s principle of optimality and is extremely s...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2021
ISSN: 1000-9361
DOI: 10.1016/j.cja.2020.11.022