System for integrated pitch and thrust control of an aircraft

Details System for integrated pitch and thrust control of an aircraft System for integrated pitch and thrust control of an aircraft

1991-11-06

1992-07-07

Barefoot, Galen

Aeronautics and astronautics

Aircraft control

Automatic

244178, 244195, 364434, 364463, B64C 1318

Patent

active

051276089

ABSTRACT:
According to the invention each of the pitch and thrust commands is a linear combination, inter alia, of the trim setting and of the speed setting, and the control provided by the aircraft joystick is pitch rate control. Protection may be provided with respect to trim, angle of incidence, and vertical load factor.

REFERENCES:
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patent: 3857535 (1974-12-01), Osder
patent: 4110605 (1978-08-01), Miller
patent: 4266743 (1981-05-01), Kelley
patent: 4420808 (1983-12-01), Diamond et al.
patent: 4598888 (1986-07-01), Beteille
patent: 4723214 (1988-02-01), Frei
patent: 4764872 (1988-08-01), Miller
patent: 4937754 (1990-06-01), Buisson et al.
patent: 4956780 (1990-09-01), Sankrithi et al.
patent: 4964599 (1990-10-01), Farineau
R. A. Hess et al., Journal of Guidance and Control and Dynamics, vol. 9, No. 6, (Nov. 1986), pages 614 to 619.
Electronics+Wireless World, vol. 96, No. 1652, (Jun. 1990), pages 470 to 478.

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