Abstract
A head up display presenting guidance information in a 3-dimensional format is considered for improving flight path control at high speed (super- and hypersonic flight). The displayed guidance information comprises a tunnel image and an aircraft position prediction which are directed at supporting the pilot to control the flight path in order to avoid conventional control technique problems caused by path-attitude decoupling. For this purpose, a predictor control law is considered which yields controlled element properties (predictor-aircraft system) requiring minimum pilot compensation. Stability and mode properties of the closed-loop system are investigated.
Original language | English |
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Pages | 515-522 |
Number of pages | 8 |
State | Published - 2000 |
Event | 7th Mini Conference on Vehicle System Dynamics, Identification and Anomalies - Budapest, Hungary Duration: 6 Nov 2000 → 8 Nov 2000 |
Conference
Conference | 7th Mini Conference on Vehicle System Dynamics, Identification and Anomalies |
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Country/Territory | Hungary |
City | Budapest |
Period | 6/11/00 → 8/11/00 |
Keywords
- Flight path control
- High speed flight
- Tunnel display