Geschwindigkeitsbeschränktes aktives Pilotsteuerorgansystem und Verfahren

Système et procédé d'interface actif de pilotage à limitation de taux de variation

Rate limited active pilot inceptor system and method

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Patent Citations (1)

    Publication numberPublication dateAssigneeTitle
    US-2005173595-A1August 11, 2005Hoh Roger H.Helicopter force-feel and stability augmentation system with parallel servo-actuator

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