发明名称 SIMULATOR FOR AIRCRAFT
摘要 PURPOSE:To secure the stability of a system sufficiently, by preventing the system from a dispersing phenomena by the control of a position input and force feedback. CONSTITUTION:The position (manupilated variable) of a control stick 1 is detected by a potentiometer 6 and the position information is applied to a computer 3'. The teering force applied to the control stick 1 is detected by a load cell 2, the force information is applied to the computer 3' as a feedback signal. The computer 3' controls a cylinder 3' on the basis of the position and force information. The cylinder 5 applies load force to the control stick 1. Since the system is stable, parameters can be easily changed in accordance with plural kinds of machines.
申请公布号 JPS5945516(A) 申请公布日期 1984.03.14
申请号 JP19820157064 申请日期 1982.09.09
申请人 MITSUBISHI JUKOGYO KK 发明人 OCHI KATSUTOSHI;MIYOSHI HIROTADA
分类号 G05D3/12;G05D3/14 主分类号 G05D3/12
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