A simple model to simulate the lateral motion during the takeoff of an aerodynamically unstable aircraft is presented. By neglecting the landing gear dynamics no additional solution of the corresponding differential equations was required. Landing gear forces were determined from the geometrical ratios of the aircraft to the ground reference line. This procedure is particularly efficient when no high frequency landing gear drive-as, e.g., during touchdown has to be taken into account. The objection free function of the control concept for an aircraft aerodynamically unstable in the lateral plane is shown.
Description of a Simple Model to Determine Landing Gear Forces During the Takeoff of Aerodynamically Unstable Aircraft Beschreibung Eines Einfachen Modells Zur Ermittlung von Fahrwerkskraeften Waehrend des Startvorgangs Eines Aerodynamisches Instabilen Flugzeugs
1981
43 pages
Report
Keine Angabe
Englisch
Verfahren zur Ermittlung der Luftgeschwindigkeit eines Flugzeugs
Europäisches Patentamt | 2018
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