FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular, to designs of unmanned aerial vehicles. The unmanned aerial vehicle comprises a centre section, fuselage, a folding wing and tail with a detachable part, vertical and horizontal tails, deflectable propulsion systems and fixed propulsion systems on a staggering beam, is equipped with a front and main support chassis and a control apparatus based on the data from inertial spatial position sensors, providing automatic stabilisation of the apparatus in a horizontal position, including in the hovering mode, wherein the inertial sensors are continuously adjusted based on GNSS data.
EFFECT: increase in the aerodynamic efficiency, reduction in the dimensions, and possibility of transporting the unmanned aerial vehicle in the folded state.
1 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
VERTICAL TAKE-OFF AND LANDING UNMANNED AIR VEHICLE | 2021 |
|
RU2767390C1 |
SMALL UNMANNED AERIAL VEHICLE | 2023 |
|
RU2812634C1 |
HIGH-SPEED UNMANNED AERIAL VEHICLE | 2021 |
|
RU2787906C1 |
UNMANNED AERIAL VEHICLE OF VERTICAL TAKE-OFF AND LANDING | 2017 |
|
RU2716391C2 |
VERTICAL OR SHORT TAKEOFF AND LANDING UNIVERSAL UNMANNED AIRCRAFT | 2015 |
|
RU2604755C1 |
DRONE AIRCRAFT (VERSIONS) | 2015 |
|
RU2613629C2 |
UNMANNED FLYING VEHICLE (VARIANTS) | 2002 |
|
RU2213024C1 |
SHORT TAKEOFF AND LANDING AIRCRAFT | 2015 |
|
RU2604951C1 |
UNMANNED AERIAL VEHICLE FOR VTOL | 2023 |
|
RU2805891C1 |
AIRCRAFT | 2012 |
|
RU2507122C1 |
Authors
Dates
2022-05-05—Published
2021-03-12—Filed