Author： Breitner M.H.
Publisher： Springer Publishing Company
ISSN： 0022-3239
Source： Journal of Optimization Theory and Applications, Vol.107, Iss.3, 2000-12, pp. : 481-503
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Abstract
Robust optimal control problems for dynamic systems must be solved if modeling inaccuracies cannot be avoided and/or unpredictable and unmeasurable influences are present. Here, the return of a future European space shuttle to Earth is considered. Four path constraints have to be obeyed to limit heating, dynamic pressure, load factor, and flight path angle at high velocities. For the air density associated with the aerodynamic forces and the constraints, only an altitude-dependent range can be predicted. The worst-case air density is analyzed via an antagonistic noncooperative two-person dynamic game. A closed-form solution of the game provides a robust optimal guidance scheme against all possible air density fluctuations. The value function solves the Isaacs nonlinear first-order partial differential equation with suitable interior and boundary conditions. The equation is solved with the method of characteristics in the relevant parts of the state space. A bundle of neighboring characteristic trajectories yields a large input/output data set and enables a guidance scheme synthesis with three-layer perceptrons. The difficult and computationally expensive perceptron training is done efficiently with the new SQP-training method FAUN. Simulations show the real-time capability and robustness of the reentry guidance scheme finally chosen.
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