A method and device for controlling a rotary wing aircraft with two rotors, in particular with impact - and swing rotor blades connected control

• 1. 具有尾部旋翼的旋翼飞行器和使尾部旋翼操作优化的方法 [P] . 中国专利： CN103253370B . 2016.01.20
• 2. 具有尾部旋翼的旋翼飞行器和使尾部旋翼操作优化的方法 [P] . 中国专利： CN103253370A . 2013-08-21
• 3. A method and device for controlling a rotary wing aircraft with two rotors, in particular with impact - and swing rotor blades connected control [P] . 德国专利： DE000001934080C . 1973-08-30

  机译： 用于控制具有两个旋翼的旋翼飞行器的方法和装置，特别是具有冲击-旋翼叶片连接控制装置的旋翼飞行器

• 4. Control system for controlling at least collective pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft [P] . 美国专利： US10654568B2 . 2020.05.19
• 5. A CONTROL SYSTEM FOR CONTROLLING AT LEAST COLLECTIVE PITCH OF ROTOR BLADES OF A MULTI-BLADE ROTOR IN A ROTARY-WING AIRCRAFT [P] . CA2970512C . 2019-06-11

  机译： 旋转翼飞机多叶片转子叶片最小共同节距控制的控制系统

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• 10. Cal/Avlabs Symposium Proceedings (3RD), 18-20 June 1969, Buffalo, New York. Aerodynamics of Rotary Wing and V/STOL Aircraft. Volume Ii. Wind Tunnel Testing. New Concepts in Rotor Control [R] . 1969

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