TTA UAVs are Chinese UAV developed by Beijing (Northern) Tian-Tu (meaning Sky Way) Aviation Technology Development Co., Ltd. (TTA, 北方天途航空技术发展有限公司). Majority of the TTA products are unmanned helicopters, but there are also fixe-wing UAV as well. Most UAV developed by TTA utilizes commercial off-the-shelf (COTS) airframes integrated with flight control systems indigenously developed by TTA.
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EH-1
EH-1 UAV is an unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids. The electrically powered micro air vehicle (MAV) is an integration of COTS airframe with flight control system developed by TTA. Specification:
EH-3
EH-3 UAV is an electrically powered unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids. EH-3 is a larger cousin of the smaller EH-1 can carry payload twice as much, and it is constructed of carbon fiber.
FH-1
FH-1 UAV is a gasoline-powered unmanned helicopter in coaxial layout, and the landing gear system consists of a pair of skids. Specification:
M4
M4 quadcopter is a multirotor developed by TTA, and the landing gear of this MAV is a pair of skids. Specification:
M6
M6 hexacopter is a multirotor developed by TTA, and the landing gear of this MAV is a pair of skids. M6 hexacopter is constructed of carbon fiber. Specification:
M8
M8 octocopter is a multirotor developed by TTA, and the landing gear of this MAV is a pair of skids. M8 octocopter is constructed of carbon fiber. Specification:
M18
M18 octodecacopter is a multirotor developed by TTA, and the landing gear of this UAV is a pair of skids. There are a total of six Y-shaped arm each with three rotors attached, two of which are at the top tips of the Y shaped arms, and the third rotor is installed in the middle of the leg of the Y shaped arm. M18 octodecacopter has been deployed in agricultural missions such as crop dusting. Specification:
RH-1
RH-1 UAV is a gasoline-powered unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids.
SH-1
SH-1 UAV is an unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids. Specification:
SP-01
SP-01 (also known as SP-1) is a fixed-wing UAV developed by TTA. This gasoline-powered MAV is in conventional layout with high-wing configuration, and it is constructed of composite material. Propulsion is provided by a two-blade propeller driven by a tractor motor mounted in the nose. Specification:
SP-02
SP-02 (also known as SP-2) is a fixed-wing UAV currently under development by TTA. SP-02 UAV is in twin-boom layout, and the twin tails are joined at the top. Propulsion is provided by a ducted propeller driven by a pusher engine mounted at the rear end of the fuselage. Specification:
VH-1
VH-1 UAV is a gasoline-powered unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids. VH-1 utilizes COTS airframes integrated with flight control systems indigenously developed by TTA. Specification:
VH-2
VH-2 UAV is an unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids. Specification:
XH-1
XH-1 is an unmanned helicopter in conventional helicopter layout, and the landing gear system consists of a pair of skids. Specification: