发明名称 ELECTRIC PROPULSION SYSTEM CONTROL APPARATUS
摘要 The present invention provides an electric propulsion system control apparatus that uses electric means alone so that effects pertaining to weight and cost are suppressed, is capable of accurate detection even when an airspeed has a binary relationship with a torque and a rotation speed of a propeller, and thereby exhibits improved detection precision and responsiveness. The electric propulsion system control apparatus drives a propulsion propeller to rotate, and is configured to estimate the airspeed from a data set stored in advance in relation to the airspeed and a propeller characteristic, and a plurality of torque and rotation speed estimation values detected under different driving conditions.
申请公布号 US2014257599(A1) 申请公布日期 2014.09.11
申请号 US201414193161 申请日期 2014.02.28
申请人 Japan Aerospace Exploration Agency 发明人 Kobayashi Hiroshi;Nishizawa Akira
分类号 B64D31/06 主分类号 B64D31/06
代理机构 代理人
主权项 1. An electric propulsion system control apparatus comprising an electric drive motor that drives a propulsion propeller to rotate, current detecting means for detecting a current of the electric drive motor, rotation speed detecting means for detecting a rotation speed of the electric drive motor, and drive control means for controlling the electric drive motor, the drive control means having: a driving force calculation unit that estimates a torque of the electric drive motor from the current detected by the current detecting means; a condition calculation unit that estimates an airspeed; and a thrust control unit that varies one or both of the torque and the rotation speed of the electric drive motor, and the condition calculation unit being configured to estimate the airspeed from a data set stored in advance in relation to the airspeed and a propeller characteristic, and a plurality of torque and rotation speed estimation values detected under different driving conditions.
地址 Tokyo JP