SY-450H Coaxial Unmanned Helicopter
SKU: MD-P00541·UAV Platforms·Bajo pedido
Vista general
SY-450H is a large coaxial helicopter product independently designed by our company, with a take-off weight of 450 kg. This model adopts a coaxial double-layer rotor design, which reduces the length of the aircraft for easy transportation; adopts a 115-horsepower turbocharged engine, which solves the problem of excessive engine power loss due to high-altitude flight, and the ceiling can reach 4,000 meters above sea level; The standard fuel tank is 120 liters, which can guarantee 4 hours of flight time. The SY-450H flight control system adopts a model-based robust control algorithm, adaptive to wind gust, high and low temperature, load changes, center of gravity changes, etc., to ensure flight accuracy and reliability in complex situations. UAV Performance Parameters: Number of paddle blades: 2 2 Load capacity: 190 kg (including fuel) Maximum take-off weight: 450 kg Engine: 115 Hp turbocharged water-cooled aero-engine Endurance time: 4 hours (standard fuel tank, load 115 kg) Start mode: remote control electric start Practical ceiling: 4000 m Autonomous functions: autonomous take-off and landing, fixed-point hovering and waypoint flight Communication mode: wireless microwave/satellite communication (optional) HY-Helicopter Flight Control System The helicopter flight controller uses industrial-grade sensors and applies modern robust control algorithms to achieve and control Helicopter attitude stability, speed, hover, autonomous take-off, autonomous landing, autonomous route flight and orhers. In addition, it can adapt to complex situations such as environmental disturbances, load changes, and gravity center shift. When installing initially Only by collecting the data of the helicopter's manual flight, the mathematical model of the helicopter can be established according to the dynamic characteristics of the controlled carrier and a robust controller can be generated. When it is installed again on a different aircraft of the same model, it is no longer necessary to repeat the parameter identification work, which greatly simplifies the system integration of the unmanned helicopter and effectively reduces the operational risk.
Especificación técnica
Specifications. Especificaciones clave: Arithmetic processing unit Redundant dual processor design /, Inertial Measurement Unit Attitude measurement accuracy: 0.2 (static)/0.3 (dynamic state), /, GPS Industrial Grade Dual Frequency GPS Receiver Professional aviation antenna / Trimble/NOVATEL GPS receiver, Position measurement accuracy 3m PCTEL aerial antenna (USA), Supports differential GPS signal input Centimeter-level differential accuracy (optional equipment), Expandable port PWM port 3-channel PWM input 3-channel PWM output / PWM input can be used to collect engine speed temperature, etc., The PWM output can be used to control user equipment such as: Spray control, PTZ control, etc., 3 RS-232 serial ports It can be used for flight control and mission equipment application control for digital Data interaction and integration (development and customization), Flight attitude control smoothness Pitch angle stability: <2 degrees /, Track control accuracy Position hovering accuracy: <1m (horizontal) 2.0m (vertical) /, Barometer Measurement accuracy: 20 cm /, Wireless data link Frequency: 840MHz, Frequency Hopping Spread Spectrum /, Line-of-sight communication distance: >15 kilometers Beijing measured 1000 meters relative altitude 35 kilometers, Wide voltage power supply 7v-17v /, Weight 980 g / Includes two GPS antennas, Dimensions 130 106 56mm /, Operating temperature -25 to +85 C /, Length 4.2 m, Height 2.1 m, Rotor diameter 5.5 m, Number of paddle blades 2 2, Empty weight 250 kg, Load capacity 190 kg (including fuel), Maximum take-off weight 450 kg, Engine 115 Hp turbocharged water-cooled aero-engine, Cruising speed 100 km/h, Endurance time 4 hours (standard fuel tank, load 115 kg), Fuel 95# gasoline, Start mode remote control electric start, Practical ceiling 4000 m, Autonomous functions autonomous take-off and landing, fixed-point hovering and waypoint flight, Route accuracy 1 m, Communication mode wireless microwave/satellite communication (optional), Attitude measurement accuracy 0.2 (static)/0.3 (dynamic state),, Accelerometer 5g,, Gyro 450 /s, Measurement data update frequency 10Hz, Dual GPS antenna heading angle measurement accuracy 1, Measurement accuracy 20 cm, Frequency 840MHz, Frequency Hopping Spread Spectrum, Transmit power 1W.
Especificación técnica — 1 groups
Especificaciones clave: Arithmetic processing unit Redundant dual processor design /, Inertial Measurement Unit Attitude measurement accuracy: 0.2 (static)/0.3 (dynamic state), /, GPS Industrial Grade Dual Frequency GPS Receiver Professional aviation antenna / Trimble/NOVATEL GPS receiver, Position measurement accuracy 3m PCTEL aerial antenna (USA), Supports differential GPS signal input Centimeter-level differential accuracy (optional equipment), Expandable port PWM port 3-channel PWM input 3-channel PWM output / PWM input can be used to collect engine speed temperature, etc., The PWM output can be used to control user equipment such as: Spray control, PTZ control, etc., 3 RS-232 serial ports It can be used for flight control and mission equipment application control for digital Data interaction and integration (development and customization), Flight attitude control smoothness Pitch angle stability: <2 degrees /, Track control accuracy Position hovering accuracy: <1m (horizontal) 2.0m (vertical) /, Barometer Measurement accuracy: 20 cm /, Wireless data link Frequency: 840MHz, Frequency Hopping Spread Spectrum /, Line-of-sight communication distance: >15 kilometers Beijing measured 1000 meters relative altitude 35 kilometers, Wide voltage power supply 7v-17v /, Weight 980 g / Includes two GPS antennas, Dimensions 130 106 56mm /, Operating temperature -25 to +85 C /, Length 4.2 m, Height 2.1 m, Rotor diameter 5.5 m, Number of paddle blades 2 2, Empty weight 250 kg, Load capacity 190 kg (including fuel), Maximum take-off weight 450 kg, Engine 115 Hp turbocharged water-cooled aero-engine, Cruising speed 100 km/h, Endurance time 4 hours (standard fuel tank, load 115 kg), Fuel 95# gasoline, Start mode remote control electric start, Practical ceiling 4000 m, Autonomous functions autonomous take-off and landing, fixed-point hovering and waypoint flight, Route accuracy 1 m, Communication mode wireless microwave/satellite communication (optional), Attitude measurement accuracy 0.2 (static)/0.3 (dynamic state),, Accelerometer 5g,, Gyro 450 /s, Measurement data update frequency 10Hz, Dual GPS antenna heading angle measurement accuracy 1, Measurement accuracy 20 cm, Frequency 840MHz, Frequency Hopping Spread Spectrum, Transmit power 1W.
Especificaciones técnicas
Specifications
- Arithmetic processing unit
- Redundant dual processor design /
- Inertial Measurement Unit
- Attitude measurement accuracy: 0.2 (static)/0.3 (dynamic state), /
- GPS
- Industrial Grade Dual Frequency GPS Receiver Professional aviation antenna / Trimble/NOVATEL GPS receiver
- Position measurement accuracy
- 3m PCTEL aerial antenna (USA)
- Supports differential GPS signal input
- Centimeter-level differential accuracy (optional equipment)
- Expandable port
- PWM port 3-channel PWM input 3-channel PWM output / PWM input can be used to collect engine speed temperature, etc., The PWM output can be used to control user equipment such as: Spray control, PTZ control, etc.
- 3 RS-232 serial ports
- It can be used for flight control and mission equipment application control for digital Data interaction and integration (development and customization)
- Flight attitude control smoothness
- Pitch angle stability: <2 degrees /
- Track control accuracy
- Position hovering accuracy: <1m (horizontal) 2.0m (vertical) /
- Barometer
- Measurement accuracy: 20 cm /
- Wireless data link
- Frequency: 840MHz, Frequency Hopping Spread Spectrum /
- Line-of-sight communication distance: >15 kilometers
- Beijing measured 1000 meters relative altitude 35 kilometers
- Wide voltage power supply
- 7v-17v /
- Weight
- 980 g / Includes two GPS antennas
- Dimensions
- 130 106 56mm /
- Operating temperature
- -25 to +85 C /
- Length
- 4.2 m
- Height
- 2.1 m
- Rotor diameter
- 5.5 m
- Number of paddle blades
- 2 2
- Empty weight
- 250 kg
- Load capacity
- 190 kg (including fuel)
- Maximum take-off weight
- 450 kg
- Engine
- 115 Hp turbocharged water-cooled aero-engine
- Cruising speed
- 100 km/h
- Endurance time
- 4 hours (standard fuel tank, load 115 kg)
- Fuel
- 95# gasoline
- Start mode
- remote control electric start
- Practical ceiling
- 4000 m
- Autonomous functions
- autonomous take-off and landing, fixed-point hovering and waypoint flight
- Route accuracy
- 1 m
- Communication mode
- wireless microwave/satellite communication (optional)
- Attitude measurement accuracy
- 0.2 (static)/0.3 (dynamic state),
- Accelerometer
- 5g,
- Gyro
- 450 /s
- Measurement data update frequency
- 10Hz
- Dual GPS antenna heading angle measurement accuracy
- 1
- Measurement accuracy
- 20 cm
- Frequency
- 840MHz, Frequency Hopping Spread Spectrum
- Transmit power
- 1W