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 (JP)
Application Number:
PCT/JP2011/054253
Publication Date:
September 01, 2011
Filing Date:
February 25, 2011
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
YAMASAKI KOICHI (JP)
YAMASAKI KOICHI (JP)
International Classes:
B64C13/00
Foreign References:
| JP2003291893A | 2003-10-15 | |||
| JPH0597095A | 1993-04-20 | |||
| JPH08183497A | 1996-07-16 |
Other References:
See also references of EP 2540621A4
Attorney, Agent or Firm:
FUJITA, Takaharu et al. (JP)
Takaharu Fujita (JP)
Takaharu Fujita (JP)
Download PDF:
Claims: