Abstract
Two types of model reference adaptive control systems for aircraft were compared. One was based on the MIT design procedure and a second based on Liapunov stability theory. The basic problem considered in this study was how well each system adapted to changes in parameters affecting aircraft performance. After considering the simulated dynamic response of an adaptively controlled aircraft at a variety of flight conditions, it was concluded that the Liapunov-based technique provided more desirable response than did the MIT system.
| Original language | English (US) |
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| Pages | 33-42 |
| Number of pages | 10 |
| State | Published - Jan 1 1974 |
| Event | Jt Autom Control Conf, 15th, Proc - Austin, TX, USA Duration: Jun 18 1974 → Jun 21 1974 |
Other
| Other | Jt Autom Control Conf, 15th, Proc |
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| City | Austin, TX, USA |
| Period | 6/18/74 → 6/21/74 |