发明名称 Optomechanical control apparatus
摘要 A control apparatus for use in a fly-by-wire flight control system. The apparatus comprises a support structure, a tube (22) mounted to the support structure for rotation about the tube lengthwise axis, at least two joysticks (18, 20) mounted to the tube, a coupling bar (24) and sensors (14, 16). Each joystick has a first end (30) adapted for gripping by an operator, a second end pivotally connected to the coupling member, and an intermediate portion (64) pivotally mounted to the tube such that the joystick is rotatable about a transverse axis (40) fixed in the tube and perpendicular to the lengthwise axis, the transverse axes of the joysticks being parallel to one another. The sensors include a two axis photodetector (44) and light emitting diodes (46) for directing a beam of radiation to a point on the photodetector. The sensor is adapted to vary the position of the point along a first axis of the photodetector as the joysticks are rotated about the lengthwise axis, and to vary the position of the point along a second axis of the photodetector as the joysticks are rotated about the transverse axes.
申请公布号 US4716399(A) 申请公布日期 1987.12.29
申请号 US19850691167 申请日期 1985.01.14
申请人 THE BOEING COMPANY 发明人 NORDLUND, LESTER H.
分类号 B64C13/12;G01D5/26;(IPC1-7):G08C9/00 主分类号 B64C13/12
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