Robust control for constant thrust rendezvous under thrust failure
نویسندگان
چکیده
منابع مشابه
Solving Optimal Continuous Thrust Rendezvous Problems with Generating Functions
The optimal control of a spacecraft as it transitions between specified states using continuous thrust in a fixed amount of time is studied using a recently developed technique based on Hamilton–Jacobi theory. Started from the first-order necessary conditions for optimality, a Hamiltonian system is derived for the state and adjoints with split boundary conditions. Then, with recognition of the ...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2015
ISSN: 1000-9361
DOI: 10.1016/j.cja.2015.02.009