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Response Characteristics of the Gyro‐Controlled Lockheed Rotor System

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The gyro of the Lockheed Rigid Rotor System fulfills two separate functions. First, it works as a mechanical autopilot which stabilizes the motion of the aircraft. Secondly, it functions as a device which counteracts and compensates external, one per rev. excitations of the rotor blade such as produced by a gust. The paper deals with the latter aspects. It describes the system and investigates the steady‐state and transient response to various types of excitations.
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Document Type: Research Article

Affiliations: Advanced Studies, Rotary Wing New Design Division, Lockheed-California Company, Burbank, California

Publication date: 1967-10-01

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  • The Journal of the American Helicopter Society is the world's only scientific journal dedicated to vertical flight technology. It is a peer-reviewed technical journal published quarterly by AHS International and presents innovative papers covering the state-of-the-art in all disciplines of rotorcraft design, research and development. (Please note that AHS members receive significant discounts on articles and subscriptions.)

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