发明名称 |
Apparatus and method for controlling aircraft, particularly remotely-controlled aircraft |
摘要 |
A remotely-controlled aircraft comprises a sensor for sensing the actual rate-of-turn of the aircraft and for generating a rate-of-turn signal proportional thereto, which signal, inherently also proportional to the actual bank-angle of the aircraft, is applied to the aileron drive as a negative feedback signal with the bank-angle command signal to thereby stabilize the bank-angle of the aircraft. The aircraft includes a further sensor for sensing the actual rate-of-climb of the aircraft and for generating a rate-of-climb signal proportional thereto, which latter signal, inherently also proportional to the actual pitch-angle of the aircfaft, is applied to the elevator drive as a negative feedback signal with the pitch-angle command signal to thereby stabilize the pitch-angle of the aircraft.
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申请公布号 |
US4964598(A) |
申请公布日期 |
1990.10.23 |
申请号 |
US19880285918 |
申请日期 |
1988.12.19 |
申请人 |
BTA AUTOMATIC PILOTING SYST |
发明人 |
BEREJIK, ZACHARIA;WALLACH, ALLON |
分类号 |
A63H30/04;B64C13/18;B64C13/20;G05D1/00 |
主分类号 |
A63H30/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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