US Patent 4283705 - Page 4 Image - System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation

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System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation

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System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 1

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 2

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 3

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 4

Page 4

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 5

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 6

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation - US Patent 4283705 - Page 4

Patent US4283705 Page 4 of 19

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