Heading reference system

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244175, 364434, 364450, 364457, G06F 1550

Patent

active

043430350

ABSTRACT:
An aircraft heading reference system including a rate gyro for sensing the yaw rate .psi. of the aircraft and producing electrical signals representative thereof; a rate gyro for sensing the pitch rate .theta. of the aircraft and producing electrical signals representative thereof; an air speed sensor for sensing air speed .nu. of the aircraft and producing electrical signals representative thereof; a roll angle computer circuit responsive to the electrical signals representative of the yaw rate, pitch rate, and air speed for determining an electrical signal representative of the roll angle .phi. according to the expression:

REFERENCES:
patent: 3281581 (1966-10-01), Lerman et al.
patent: 3683378 (1972-08-01), Polhemus
patent: 3979090 (1976-09-01), Brickner et al.
patent: 4106094 (1978-08-01), Land

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