Distributed power multi-rotor VTOL (vertical take off and landing) aircraft and control method thereof
A vertical take-off and landing, flight control technology, applied in the aerospace field, can solve problems such as loss of lift, loss of control of aircraft flight attitude, loss of human, material and financial resources, etc., to achieve the effect of improving reliability and reducing the risk of crashes
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Embodiment 1
[0066] Embodiment 1: Distributed power multi-rotor vertical take-off and landing aircraft with four lift power units
[0067] Such as Figure 1-4 As shown, it is the structural representation of the distributed power multi-rotor vertical take-off and landing aircraft and the structural representation of the power unit of Embodiment 1 of the present invention; On the airframe, several lift power units and thrust power units installed in the fairing 1, as well as the central flight control computer system.
[0068] Wherein the fairing 1 is used to reduce the air resistance when the aircraft is in level flight. At the same time, in the level flight state, the fairing can also provide lift.
[0069] In this embodiment, four lift power units are set as an example, which are respectively a front lift power unit 2, a rear lift power unit 9, a left lift power unit 13 and a right lift power unit 8. The four lift power units are evenly Set in the four directions of the front, rear, l...
Embodiment 2
[0145] Embodiment 2: Distributed power multi-rotor vertical take-off and landing aircraft with five lift power units
[0146] Such as Figure 5-7 As shown, it is a schematic structural diagram of the distributed power multi-rotor vertical take-off and landing aircraft of the second embodiment of the present invention; the difference between this embodiment and the previous embodiment is that the aircraft of this embodiment has five lift power units: front lift Power unit 2, left front lift power unit 30, right front lift power unit 27, left rear lift power unit 29 and right rear lift power unit 28, five lift power units in total, evenly arranged on the aircraft body, adjacent two lift power units The included angles between the lines connecting the geometric center of the power unit to the center of gravity of the aircraft are equal.
[0147] The structure of each lift power unit is the same as that of the front lift power unit 2, and is the same as that of the lift power uni...
Embodiment 3
[0199] Embodiment 3: Distributed power multi-rotor vertical take-off and landing aircraft with six lift power units
[0200] Such as Figure 8-Figure 11 As shown, it is a schematic structural diagram of a distributed multi-rotor vertical take-off and landing aircraft according to Embodiment 3 of the present invention: the difference between this embodiment and the preceding embodiments is that this embodiment includes six lift power units: front lift power unit 2, The left front lift power unit 30, the right front lift power unit 27, the left rear lift power unit 29, the right rear lift power unit 28, and the rear lift power unit 9 are evenly arranged on the aircraft body. The angles between the lines connecting the geometric centers of two adjacent lift power units to the center of gravity of the aircraft are equal. The structure of each lift power unit is the same as that of the front lift power unit 2 .
[0201] Wherein, the left side thrust power unit 14 and the right si...
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