Title:
CONTROL SYSTEM OF AIRCRAFT, METHOD FOR CONTROLLING AIRCRAFT, AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2011/105536
Kind Code:
A1
Abstract:
In order to enable stable flight without needing a complicated throttle operation by a pilot even when part or all of a control surface has malfunctioned, a control system of an aircraft is provided with a calculation means (15) for calculating a thrust command control signal for controlling engine thrust and a control surface angle command control signal for controlling a control surface on the basis of state information relating to the body of the aircraft and an operation command signal from an operation end, an engine driving means (17) for driving an engine on the basis of the thrust command control signal, and a control surface driving means (16) for driving each control surface on the basis of the control surface angle command control signal.
Inventors:
YAMASAKI, Koichi (C/O MITSUBISHI HEAVY INDUSTRIES LTD, 16-5, Konan 2-chome, Minato-k, Tokyo 15, 〒1088215, JP)
Application Number:
JP2011/054253
Publication Date:
September 01, 2011
Filing Date:
February 25, 2011
Export Citation:
Assignee:
MITSUBISHI HEAVY INDUSTRIES, LTD. (16-5, Konan 2-chome Minato-k, Tokyo 15, 〒1088215, JP)
三菱重工業株式会社 (〒15 東京都港区港南二丁目１６番５号 Tokyo, 〒1088215, JP)
三菱重工業株式会社 (〒15 東京都港区港南二丁目１６番５号 Tokyo, 〒1088215, JP)
International Classes:
B64C13/00
Attorney, Agent or Firm:
FUJITA, Takaharu et al. (37F The Landmark Tower Yokohama, 2-2-1 Minatomirai, Nishi-ku, Yokohama-sh, Kanagawa 37, 〒2208137, JP)
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Claims: