1979
DOI: 10.2514/3.55827
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Automatic Rollout Control of the 747 Airplane

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“…The integral of Dy should also be fed back to eliminate the steady-state error when there is a constant crosswind. In addition, the lateral velocity Dv by , the yaw rate Dr and the yaw angle Dc will all be fed back to improve the dynamic characteristics (Cotter and Cohen, 1977).…”
Section: Directional Control Law Designmentioning
confidence: 99%
“…The integral of Dy should also be fed back to eliminate the steady-state error when there is a constant crosswind. In addition, the lateral velocity Dv by , the yaw rate Dr and the yaw angle Dc will all be fed back to improve the dynamic characteristics (Cotter and Cohen, 1977).…”
Section: Directional Control Law Designmentioning
confidence: 99%