Abstract
A control approach was developed for nonlinear systems based on aircraft modeling, and control performance is based on the accuracy of the model. In the actual aircraft implementation, a neural network is substituted for the model and trained offline to produce the same results. A methodology is developed to validate both the network and the overall controller as meeting performance and reliability requirements. Development of a multi-axis controller using this methodology with a fuzzy controller for reconfiguration is presented. Computer simulations to test the methodology on a simple airfoil and a pitch axis flight controller are also reported.
Original language | English |
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Pages | 401-409 |
Number of pages | 9 |
DOIs | |
State | Published - 1994 |
Event | Guidance, Navigation, and Control Conference, 1994 - Scottsdale, United States Duration: 1 Aug 1994 → 3 Aug 1994 |
Conference
Conference | Guidance, Navigation, and Control Conference, 1994 |
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Country/Territory | United States |
City | Scottsdale |
Period | 1/08/94 → 3/08/94 |