| 摘要 |
FIELD: control systems; devices for determination of take- off mass of aircraft. SUBSTANCE: device includes control panel, air signal meter, power plant parameter meter, pitch angle meter, angle-of-attack meter, wing high-lift devices position meter, control surface position meter, lift-off sensor, computer, storage unit, logic unit, indicator and recorder. Mass is determined by calculating relationship of forces acting on aircraft at lift-off. EFFECT: enhanced accuracy of determination of mass. 3 dwg |
