System for integrated pitch and thrust control of an aircraft

Aeronautics and astronautics – Aircraft control – Automatic

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Details

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
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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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