Patent ID: 8352098

Claim:
A flight control system comprising: a first sensor configured to detect a force applied from an outside to a first control lever; a link mechanism configured to mechanically connect said first control lever to a second control lever different from said first control lever, and transmit a force from said first control lever to said second control lever; a second sensor configured to detect a force transmitted from said first control lever to said link mechanism; a flight control computer configured to include a sticking determination portion which determines whether or not sticking arises in said first control lever on the basis of said force detected by said first sensor and said force detected by said second sensor; and a separation unit configured to disconnect said link mechanism on the basis of a separation command to separate a connection between said first control lever and said second control lever, wherein said sticking determination portion outputs said separation command to said separation unit when determining that said sticking arises in said first control lever.