octacopter
An octa-rotor aircraft and a technology for an aircraft, applied in the field of aircraft, can solve problems such as weak yaw capability, and achieve the effects of improving yaw capability, reducing energy consumption, and improving yaw capability
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specific Embodiment approach 1
[0044] Specific implementation mode one, as figure 1 As shown, set the center of mass of the aircraft as the origin o of the body coordinate system, the x-axis, y-axis, and z-axis are perpendicular to each other, the y-axis is to the left in the paper, the z-axis is perpendicular to the outside of the paper, and the x-axis is in the paper Up, the xoy plane is divided into four quadrants, the x-axis direction is set as the nose direction of the aircraft, and the z-axis is along the longitudinal plane of the aircraft, pointing upward.
[0045]Four equal-length support arms are detachably mounted on the body 1 through a hinged structure, and each support arm is connected to the avionics system 2. The first support arm 401 and the third support arm 403 are in the body coordinate system xoy plane. The projections of the second support arm 402 and the fourth support arm 404 on the xoy plane of the body coordinate system are collinear, and the projections of the first support arm 401...
specific Embodiment approach 2
[0054] Specific embodiment two, such as image 3 As shown, set the center of mass of the aircraft as the origin o of the body coordinate system, the x-axis, y-axis, and z-axis are perpendicular to each other, the y-axis is to the left in the paper, the z-axis is perpendicular to the outside of the paper, and the x-axis is in the paper Up, the xoy plane is divided into four quadrants, the x-axis direction is set as the nose direction of the aircraft, and the z-axis is along the longitudinal plane of the aircraft, pointing upward.
[0055] Four equal-length support arms are detachably mounted on the body 1 through a hinged structure, and each support arm is connected to the avionics system 2. The first support arm 401 and the third support arm 403 are in the body coordinate system xoy plane. The projections of the second support arm 402 and the fourth support arm 404 on the xoy plane of the body coordinate system are collinear, and the projection of the first support arm 401 and...
specific Embodiment approach 3
[0063] Specific embodiment three, such as Figure 5 As shown, set the center of mass of the aircraft as the origin o of the body coordinate system, the x-axis, y-axis, and z-axis are perpendicular to each other, the y-axis is to the left in the paper, the z-axis is perpendicular to the outside of the paper, and the x-axis is in the paper Up, the xoy plane is divided into four quadrants, the x-axis direction is set as the nose direction of the aircraft, and the z-axis is along the longitudinal plane of the aircraft, pointing upward.
[0064] Four equal-length support arms are detachably mounted on the body 1 through a hinged structure, and each support arm is connected to the avionics system 2. The first support arm 401 and the third support arm 403 are in the body coordinate system xoy plane. The projections of the second support arm 402 and the fourth support arm 404 on the xoy plane of the body coordinate system are collinear, and the projections of the first support arm 401...
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