Aeronautics and astronautics – Aircraft control – Automatic
Patent
1995-05-15
1997-12-02
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft control
Automatic
B64C 1316
Patent
active
056927088
ABSTRACT:
A method and apparatus for managing the trim of an airplane stabilizer whose elevator is controlled by a highly augmented elevator control law is disclosed. The augmented portion of the elevator command ##EQU1## is evaluated(13) to determine if it is above or below a variable threshold whose magnitude is dependent on airspeed. Portions above or below the threshold are integrated (15) to determine if the augmented portion of the elevator command is rapidly or slowly diverging. A stabilizer trim command is rapidly produced if the augmented portion of the elevator command is rapidly diverging and produced more slowly if the augmented portion is slowly diverging. The stabilizer trim command causes the production of a trim up or trim down command (25/27) depending upon whether the stabilizer needs to be moved up or down. Trim up commands (25) are inhibited under certain conditions, such as when the tail of the airplane is near the ground, when the airplane angle of attack is above the point where further nose up trim would be ineffective, or when the stabilizer trim limit has been exceeded. Trim down commands (27) are inhibited when the stabilizer trim down limit has been exceeded. Trim up and trim down commands are also inhibited when the command would drive the stabilizer out of fair with the elevator. Finally, provision is made for direct stabilizer trim control by the pilot of the airplane in the event that the elevator is limited and, thus, the stabilizer is required to produce additional pitch response.
REFERENCES:
patent: 3945593 (1976-03-01), Schanzer
patent: 5079711 (1992-01-01), Lambregts et al.
patent: 5127608 (1992-07-01), Farineau et al.
patent: 5527002 (1996-06-01), Bilange et al.
Coleman Edward E.
McCuen Michael S.
Najmabadi Kioumars
Barefoot Galen L.
The Boeing Company
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