Systems and methods for controlling aircraft flaps and spoilers
A technology for spoilers and aircraft, which is used in aircraft control, indicating the direction of movable elements of aircraft, aircraft parts, etc., and can solve problems such as reducing system versatility, increasing system complexity and weight, etc.
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[0013] SUMMARY OF THE INVENTION Systems and methods are described for controlling aircraft flaps and spoilers, including configurations in which actuation of the flaps is mechanically independent of actuation of the spoiler. Certain specific details are set forth in the ensuing description and in Figures 2-6 to provide a thorough understanding of various embodiments of the invention. Well-known structures, systems, and system-related methods have not been shown or described in detail to avoid unnecessarily obscuring the description of the various embodiments of the invention. Furthermore, those skilled in the art will appreciate that additional embodiments of the invention may be practiced without some of the details described below.
[0014] Many embodiments of the invention described below may employ a controller in the form of computer-executable instructions, including programs executed by a programmable computer or, alternatively, by a non-programmable electronic device. ...
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