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- W2679344251 abstract "Abstract The paper deals with entry guidance of a shuttle orbiter. First, it is necessary to set the trajectory on a reference curve given in the speed/acceleration plane. This first problem can be solved with an open loop optimization. The second step, which is the main contribution of this paper, consists in tracking a reference profile. According to the framework of non linear control theory, a linearizing feedback is obtained after a change of variables in the state equations. The obtained results show the efficiency of this approach compared to the classical PID control policies given in the relevant litterature" @default.
- W2679344251 created "2017-06-30" @default.
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- W2679344251 date "1993-07-01" @default.
- W2679344251 modified "2023-09-25" @default.
- W2679344251 title "Nonlinear Control Approach to Reentry Guidance of a Spacecraft" @default.
- W2679344251 doi "https://doi.org/10.1016/s1474-6670(17)48857-4" @default.
- W2679344251 hasPublicationYear "1993" @default.
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