公开(公告)号：US08855838B2

公开(公告)日：2014-10-07

申请号：US13381197

申请日：2009-10-28

Applicant: Bernard Berthier

Inventor： Bernard Berthier

IPC: G06F19/00 ,  G05D1/00 ,  G05D1/08 ,  G05D3/00 ,  B64C39/02 ,  B64C31/036

CPC classification number: B64C31/036 ,  B64C39/024 ,  B64C2201/105 ,  B64C2201/107

Abstract: The invention relates to an automatic takeoff method for an aircraft with a flexible airfoil, comprising a carriage suspended by rigging lines from an airfoil. According to said method: —said carriage is provided with an autopilot controlling actuators that control said rigging lines; —said airfoil is provided with an airfoil attitude sensor, comprising a biaxial accelerometer and a biaxial rate gyro, capable of defining the position of an airfoil reference frame in relation to the ground, and means for communicating with said autopilot; —during takeoff, information is received from said airfoil attitude sensor and transmitted to said autopilot for the purpose of controlling said actuators. The invention also relates to an airfoil for the implementation of said method, comprising an airfoil attitude sensor with an inertial unit with a biaxial accelerometer and a biaxial rate gyro, and means for communicating with an autopilot. The invention further relates to an aircraft comprising such an airfoil.

Abstract translation: 本发明涉及一种具有柔性翼型的飞行器的自动起飞方法，该飞行器包括通过从翼型装配线路悬挂的滑架。 根据所述方法：托架具有控制所述索具线的自动驾驶控制致动器; 翼面设置有翼型姿态传感器，包括双轴加速度计和双轴率陀螺仪，其能够定义相对于地面的翼型参考框架的位置，以及用于与所述自动驾驶仪通信的装置; 在起飞时，为了控制所述致动器，从所述翼型姿态传感器接收信息并传送到所述自动驾驶仪。 本发明还涉及一种用于实现所述方法的翼型件，包括具有带有双轴加速度计和双轴率陀螺仪的​​惯性单元的翼型姿态传感器和用于与自动驾驶仪通信的装置。 本发明还涉及一种包括这种翼型的飞行器。

公开(公告)号：US20120109427A1

公开(公告)日：2012-05-03

申请号：US13381197

申请日：2009-10-28

Applicant: Bernard Berthier

Inventor： Bernard Berthier

IPC: G05D1/00 ,  B64C31/036

CPC classification number: B64C31/036 ,  B64C39/024 ,  B64C2201/105 ,  B64C2201/107

Abstract: The invention relates to an automatic takeoff method for an aircraft with a flexible airfoil, comprising a carriage suspended by rigging lines from an airfoil. According to said method:—said carriage is provided with an autopilot controlling actuators that control said rigging lines;—said airfoil is provided with an airfoil attitude sensor, comprising a biaxial accelerometer and a biaxial rate gyro, capable of defining the position of an airfoil reference frame in relation to the ground, and means for communicating with said autopilot;—during takeoff, information is received from said airfoil attitude sensor and transmitted to said autopilot for the purpose of controlling said actuators. The invention also relates to an airfoil for the implementation of said method, comprising an airfoil attitude sensor with an inertial unit with a biaxial accelerometer and a biaxial rate gyro, and means for communicating with an autopilot. The invention further relates to an aircraft comprising such an airfoil.

Abstract translation: 本发明涉及一种具有柔性翼型的飞行器的自动起飞方法，该飞行器包括通过从翼型装配线路悬挂的滑架。 根据所述方法：托架提供有控制所述索具线的自动驾驶控制致动器;所述翼型件设置有翼型姿态传感器，包括双轴加速度计和双轴率陀螺仪，能够限定翼型的位置 相对于地面的参考框架和用于与所述自动驾驶仪通信的装置; - 在起飞时，从所述翼型姿态传感器接收信息并传送到所述自动驾驶仪，以控制所述致动器。 本发明还涉及一种用于实现所述方法的翼型件，包括具有带有双轴加速度计和双轴率陀螺仪的​​惯性单元的翼型姿态传感器和用于与自动驾驶仪通信的装置。 本发明还涉及一种包括这种翼型的飞行器。