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Abstract
The development, verification, and validation of flight control software for aircraft is characterized by high demands on accuracy, reliability and efficiency. Such processes cover all stages from first simulations to final flight test. The respective environment is described here on the basis of the experimental aircraft X-31A. Besides the applied hard- and software, special emphasis is given to simulation models and their updates, being marked by two new approaches: the use of nearly identical simulation software during the whole development and verification process and update of integrated simulation models due to special flight tests by means of global model system identification.
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