Monday, September 24, 2012

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HK401B INSTRUCTION MANUAL PDF

HK401B is a gyro with function of dual rate and head lock, which designed for helicopters specially. HK401B adopts AVCS(Angular Vector Control System), which makes the function of head lock more outstanding and steady. AVCS system: Since rudder trim changes caused by wind and other meteorological changes, and varieties of helicopter attitude changes are automatically cancelled, tail rudder operation becomes easy, making it perfect for 3D flight.

HK401B speciļ¬cations: Digital proportional R/C system Operating voltage: 4.8V ~6V(common for receiver) Operating temperature: -10 ~+45 Dimensions: 28×28×20 mm Operating current: 80mA Functions: > Minimizes changes in an aircraft's attitude by wind etc > Angular acceleration commands used > Sensor vibration proofing > Simple sensitivity adjustment

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