发明名称 Rotor aircraft e.g. civil helicopter, has controller changing moving condition of aircraft in direction of deflection with respect to deflection of handle, where change measurement is increased with deflection measurement
摘要 <p>The aircraft has a controller generating control commands to driving and steering devices. A handle (1) moves from a normal position opposite to the aircraft in translational directions (4, 6, 7) and rotational directions (5, 8, 9). The controller changes the moving condition of the aircraft in the direction of the deflection with respect to the deflection of the handle, where the change measurement is increased with the deflection measurement, and a restoring force acts on the handle in the normal position, where the measurement of the force is increased with the deflection of the handle.</p>
申请公布号 DE102008028365(A1) 申请公布日期 2009.12.24
申请号 DE20081028365 申请日期 2008.06.13
申请人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. 发明人 WILKE, BASTIAN
分类号 B64C27/56;G06G7/72 主分类号 B64C27/56
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