BY HOEYCOMB AEROSPACE TECHNOLOGIES HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV
Content SYSTEM SPECIFICATI- ON TYPICAL USING PROCESS OVERVIEW SUBSYSTEM SPECIFICATI- ON
1 OVERVIEW System characteristics Flightmode Typicalareasofapplication
System characteristics Gas-battery hybrid system helps to achieve more than 120 minutes endurance Can be mounted with different payloads to accomplish multi-tasks such as HD video capture and real-time return, 3D mapping, projectile throwing and air propaganda Fully autonomous flight capability Be equipped with omni-directional millimeterwave radar avoidance system and parachute selfprotect system for emergency
Flight Mode Autonomous flight: Fly according to a preset path planning, flight route planning which can be modified through ground station in real time. Remotecontrol flying: Use the remote controller for flight control
Typical areas of application Surveying and mapping (with tilt camera): processes acquired aerial photographs into 3D map with geographical information. Investigation, monitoring (configured with tactical micro electro-optical pod): goal seeking, locking, tracking, target video realtime transmission to the ground control station.
2 SYSTEM SPECIFICATION System composition General technical specifications
System Composition
General technical specifications Control radius: 7km; (remote link configured according to the needs) standard payload weight: 3kg Operating temperature: -40c ~ +55 Cruise speed: 5-8M/s Maximum payload weight: 4kg Endurance: 120min Service ceiling: 3000m; ( height from the ground) Maximum flight speed: 10m/s Max takeoff weight: 18kg standard payload weight: 3kg Wind resistance: 6 level Take off prep time: 5min; (daytime,2 operators) Clear and withdraw Time: 3min; (daytime,2 operators)
3 Subsystem Specification Flying platform Power plant Electricalsystem Flight control system Communications and data link system Groundcontrolstation, andgroundsupport equipment Suitable ambient environment for using and storage
Dynamical systems Gasoline-electric hybrids Flying Platform The maximum takeoff weight 18kg Standard payload 3kg Flight systems Axis Spread 1.45m Body dimensions (m) 1.45 1.45 0.5 Body material Endurance time Normal cruise speed Maximum cruise speed Carbon fiber composite material 120Minutes 0-8m/s 12m/s Flying height 0-3000m HC-330 Six-rotor UAV adopts x-type four-rotor layout, with fully enclosed fuselage design, can effectively prevent debris getting into the inside. It adopts horizontal folding design with the arms for easy transportation and small space occupation, the diagonal wheelbase is 1.45m. Carbon fiber composite material is applied in the full-aircraft. Power plant HC-8012Kv95DCBrushless motor
Power plant Transform the power into 3 phase AC power Gas-Battery hybrid generator Provide power to Airborne battery pack ES C Transform the electricity power in the battery pack into kinetic power to propellers Drive motor
Electrical system Components Back battery pack: 3 4S1800mAh battery Distribution board Power panel Airborne cable The main function of the electrical system is to supply power to the airborne equipments and achieve effective connection and transmission of the signal among different equipments.
flight control system HCAP-001(1) It supports Hover Autonomoustaking-off and landing Planning routes Switching flight mode in real time Control the flight status such as attitude, altitude, heading and position of the aircraft and achieve stable and reliable automatic flight External radio It adopts differential GPS with an location accuracy of 2 cm Can be defined with multiple no-fly zone restriction
flight control system HCAP-001(2) Table 2. HCAP-001 multi-rotor flight control parameters DGPS Receiver 3 Axis gyro 3 -Axis accelerometer 3 Axis magnetic sensor DGPS/SINS Precision Air pressure sensor Data update rate receivable RTK Positioning accuracy Cold start lock star time Range Angle random walk 1σ Noise density rate (25Hz, no filtering) Range Random walk speed 1σ Noise density (no filter) Range Heading accuracy Attitude Heading High-precision Static pressure range High resolution Dynamic pressure Maximum supported air speed 5 Hz Differential GPS GPS/GLONASS/BeiDou 1cm+1ppm <30s ±300deg/s 1.0deg/hr 0.02deg/s/sqrt(Hz) rms ±18g 0.076m/s/sqrt(hr) 0.06mg/sqrt(Hz) rms ±8 Gauss 2.0deg rms 0.5 1.5 2cm rms 20 Kpa -103.35Kpa 0.1m 0-13.78Kpa 150m/s (540km/h)
communications and data link system HCDL-020(1) Airborne data terminal performance indicators are as follows: Specifications: Video input connector: HDMI Control signal interface: UART, USB2.0 Encoding format: h. 264 Channel bandwidth: 10MHz Input voltage: 5V 15V, the input current >2A Dimensions: 60mmx70mmx20mm (LxWxH)
Performance parameter 1. Transmitter module communications and data link system HCDL-020(2) Supported resolution: 1080P@60, 1080P@30, 1080i@60, 1080i@50 720P@30 720i@60 Transmit power: 100mW 300mW(software adjustable) Power consumption: <5W Operating temperature: -40 -+80
communications and data link system HCDL-020(3) 2. Receiver module Propagation delay: <200ms Video from: 10km Power consumption: <5W Operating temperature: -40 -+80
Ground control station, and ground support equipment(1) The ground control station mainly implement remote control, telemetry, tracking, positioning and mission planning for the UAV It can achieve remote control for the UAV and realize monitoring, recording and distribution for the payloads information. It can be easily carried and operated by single person and can also be loaded or deployed in the front line to be used alone.
Ground control station, and ground support equipment(2): the interface of the ground station 1 Quick access tool bar 2 Electrical Map 3 Key parameters 4 Key operations 5 Flight instruments
Other divices and equipment Futaba T8FG Remote control Honeycomb portable mobile ground terminal Carrying Case Charger
4 Typical using process
HONEYCOMB AEROSPACE TECHNOLOGIES(Beijing) CO.,LTD Thanks Contact us: Niki Wang 15810112173 Website: www.honeycombs.com.cn Email: info@honeycombs.com.cn