G - Physics – 06 – G
Patent
G - Physics
06
G
343/119
G06G 7/32 (2006.01) G01C 21/20 (2006.01)
Patent
CA 1042092
A B S T R A C T A method and apparatus for computing vertical track angle is provided which uses the output from an area navigation computer and an altitude differential to make the desired com- putation. The apparatus includes suitable circuitry for pro- ducing a null at an output connection node point. Output of an integrator signal generating circuit means, after the null point is achieved, is the desired vertical track angle. Any aircraft deviation from the correct flight path after vertical track angle computation is completed is represented by an error signal at the output node which may be visually displayed.
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