| 摘要 |
#CMT# #/CMT# The method involves transmitting two control commands of mobile bodies (10) e.g. spoiler and aileron, to actuating units (8, 12) when activation conditions are fulfilled. Deviation of wind is compared with a preset threshold value. Auxiliary control command of the body (14) is calculated using values of flight parameters. One of the commands is transmitted to the unit (12) when the conditions are fulfilled and the deviation is greater than or equal to the value so that the body (14) is subjected to total control command corresponding to sum of the command and auxiliary control command. #CMT# : #/CMT# An independent claim is also included for device for attenuating effects of vertical turbulence met by an aircraft during flight, comprising a mobile body. #CMT#USE : #/CMT# Method for attenuating effects of vertical turbulence on an aircraft (claimed) i.e. transport aircraft, during flight. Can also be used for a military aircraft, civil aircraft and commercial aircraft. #CMT#ADVANTAGE : #/CMT# The method permits the auxiliary control command to act indirectly on dynamic lift at the centre of gravity of the aircraft so as to increase load factor authority, thus minimizing amplitude of vertical load factor generated by vertical turbulence, and hence permitting optimized and accurate attenuation of effects generated by the vertical turbulence and reducing variations of altitude. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a block diagram of a device for attenuating effects of vertical turbulence on aircraft. 5 : Calculation unit 8, 12 : Actuating units 10, 14 : Mobile bodies 16 : Verification unit 18 : Transmission unit. |
