The thesis presents an approach to develop elementary math functions for flight control systems. Here, especially the integration in the whole development process is considered. Therefore, the precision of the implemented functions is shown with formal proofs. The validity of ranges is shown via a runtime error analysis. The timing aspects are considered with a two level worst case execution time analysis. A first analysis is executed to select an implementation for the basic math function. The second analysis is executed on the complete integrated software.
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The thesis presents an approach to develop elementary math functions for flight control systems. Here, especially the integration in the whole development process is considered. Therefore, the precision of the implemented functions is shown with formal proofs. The validity of ranges is shown via a runtime error analysis. The timing aspects are considered with a two level worst case execution time analysis. A first analysis is executed to select an implementation for the basic math function. The...
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