Pitch control system for aircraft

Details Pitch control system for aircraft Pitch control system for aircraft

1991-04-24

1992-05-12

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft control

244 90A, 244181, 244203, 244213, B64C 934, B64C 1316, G05D 108

Patent

active

051120097

ABSTRACT:
A pitch control system for an aircraft flying at a Mach number greater than 0.7 and including a horizontal plane that is adjustable in deflection and air brakes having a nose-down effect. According to the invention, the system comprises:

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