Aircraft control systems
A control system, aircraft technology, applied in the direction of aircraft control, control/regulation system, mechanical control device, etc., can solve problems such as increased cost and complexity, different system characteristics and requirements, etc.
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[0045] Further details, aspects and embodiments of the invention will now be described, by way of example only, with reference to the accompanying drawings. Elements in the figures are illustrated for simplicity and clarity and have not necessarily been drawn to scale. Like reference numerals have been included in the various drawings for ease of understanding.
[0046] figure 1 A schematic diagram representing an aircraft control system showing only the relevant parts of the system. The input controls 10a-10d represent inputs used by the operator, eg, side stick shafts, throttle, rudder pedals, joysticks, etc., which are commonly referred to as receptors. Outputs 11a-11d represent aircraft controls such as ailerons, elevators, engines, rudder, nose wheel steering and brakes. Processing system 12 receives signals from input controls 10a-10d, processes the signals, and outputs control signals to outputs 11a-11d. Processing system 12 may be a computer system connected to all...
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