Product Introduction:

HWA-ZC is an oil electric hybrid vertical takeoff and landing fixed wing unmanned aerial vehicle, equipped with advanced oil powered engines and powerful power drive. It combines the advantages of electric rotors and adopts a hybrid oil powered driving method. It also has the ability to perform vertical takeoff and landing for quadcopters and fast cruising for fixed wing aircraft, and can adapt to various complex takeoff and landing environments. According to the design of multi payload missions, there is a super large payload compartment under the fuselage, which can carry a mission payload of no less than 15kg, truly achieving multi-purpose use of one aircraft for field operations. Can be used for surveying, power line patrol, target drones and other scenarios.

1Drone platform

2、 Flight Control System

The basic function of the flight control system is to control the flight attitude of the drone, reach the target position according to the given control strategy, complete the pre-set flight task, and exchange data, set and change tasks with the ground station. The flight control system of this drone has undergone thousands of algorithm iterations, ensuring stable and reliable flight control. The main technical indicators are as follows:

（1) Positioning accuracy: 1.5m；

（2) Height measurement accuracy: 3.5m；

（3) Heading measurement accuracy: 2.5 °;

（4) Attitude measurement accuracy: 1.5 °

（5) Attitude and heading measurement range: ± 180 °.

3、 Ground station system

The ground station can control the altitude, attitude, heading, and position of the drone, and can monitor the real-time flight status such as altitude, airspeed, heading, attitude, position, battery voltage, etc. It can design and adjust the target drone flight plan before and during the drone flight. In case of emergency situations such as fuel depletion or low battery voltage, it can autonomously return. In summary, ground stations have the following functions:

（1) It can automatically control the trajectory or manually control the trajectory;

（2) Display the flight status parameters of the drone;

（3) Real time display of drone position, preset trajectory, and flight path information;

（4) Capable of real-time recording of flight data and ground station related information;

（5) Remote control of infrared source ignition or timed ignition at ground station setting time can be achieved through data link; Rotation of the pod, etc;

（6) Capable of controlling the flight of a 6-machine formation at one station.

4、 Environmental adaptability

（1）Working temperature:- 30℃～+60℃；

（2）Storage temperature:- 45℃～+65℃；

（3）Landing site: 8m * 8m flat ground;

（4）Wind resistance: Level 7;

（5）Storage life: The lifespan of the product should not be less than 6 years when stored in a warehouse with 85% humidity inside the packaging box;

（6）Electromagnetic compatibility: according to GJB151A-97、GJB1489A-2005 conducts electromagnetic compatibility design to ensure the entire systemelectromagnetismCompatible with work.

5、 Usability

（1）Continuous takeoff interval: 10 minutes;

（2）The whole machine can be quickly assembled by hand, taking time8minute;

（3）The rotor take-off and landing arm and the hanging power battery can be quickly disassembled and assembled.

6、 Task payload

7、 Reliability

The reliability of airborne equipment operation shall not be less than0.99.