Method and apparatus for controlling an unmanned symmetric...

G - Physics – 05 – D

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G05D 1/10 (2006.01) B64C 27/54 (2006.01) G05D 1/08 (2006.01)

Patent

CA 2241114

Apparatus for controlling an unmanned generally aerodynamically symmetric aircraft includes detection means for detecting the presence of misalignment between the horizontal component of the center of gravity vector and the horizontal component of the direction of flight vector and further includes rotation means for rotating the aircraft to align the horizontal components of the vectors.

Cette invention concerne un appareil conçu pour commander un aéronef télépiloté généralement symétrique d'un point de vue aérodynamique. Ledit appareil comporte d'une part, un organe de détection conçu pour détecter l'existence d'un mauvais alignement entre la composante horizontale du vecteur de centre de gravité et la composante horizontale du vecteur de direction de vol et d'autre part, un organe de rotation conçu pour faire pivoter l'aéronef de façon à aligner les composantes horizontales de ces vecteurs.

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