Equipment was designed to be added or retrofitted to Boeing 707/720 airplanes to enable low approach and automatic landings to be made under conditions of low visibility as part of regular airline operations; major elements of system such as autopilot, yaw damper, approach and flare couplers and auto-throttle system are described in relation to their effects on performance and safety; details of monitoring and automatic test subsystems and test procedures used to evaluate system design.
Boeing/bendix automatic landing system for 707 aircraft
SAE-NASA -- Aerospace Vehicle Flight Control Conference -- Proc
Proceedings of the SAE-NASA Aerospace Vehicle Flight Control Conference ; 1965 Landing
1965
12 pages
Conference paper
English
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The Boeing/Bendix Automatic Landing System for the 707 Aircraft
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