Especificações
Aircraft
| Takeoff Weight | 1391 g |
|---|---|
| Diagonal Distance | 350 mm |
| Max Service Ceiling Above Sea Level | 19685 ft (6000 m) |
| Max Ascent Speed | 6 m/s (automatic flight); 5 m/s (manual control) |
| Max Descent Speed | 3 m/s |
| Max Speed | 31 mph (50 kph)(P-mode) 36 mph (58 kph)(A-mode) |
| Max Flight Time | Approx. 30 minutes |
| Operating Temperature Range | 32° to 104° F (0° to 40℃) |
| Operating Frequency | 2.400 GHz to 2.483 GHz (Europe, Japan, Korea) 5.725 GHz to 5.850 GHz (United States, China) |
| Transmission Power (EIRP) | 2.4 GHz CECE (Europe) / MIC (Japan) / KCC (Korea) ：<20 dBm5.8 GHz SRRC（China） / FCC（United States）/(Taiwan,China)：<26 dBm |
| Hover Accuracy Range | RTK enabled and functioning properly： Vertical：±0.1 m；Horizontal：±0.1 mRTK disabled Vertical：±0.1 m（with vision positioning ）； ±0.5 m（with GNSS positioning） Horizontal：±0.3 m（with vision positioning）; ±1.5 m（with GNSS positioning） |
| Image Position Offset | The position of the camera center is relative to the phase center of the onboard D-RTK antenna under the aircraft body’s axis:(36, 0, and 192 mm) already applied to the image coordinates in Exif data. The positive x, y, and z axes of the aircraft body point to the forward, rightward, and downward of the aircraft, respectively. |
Mapping Functions
| Mapping Accuracy ** | Mapping accuracy meets the requirements of the ASPRS Accuracy Standards for Digital Orthophotos Class Ⅲ ** The actual accuracy depends on surrounding lighting and patterns, aircraft altitude, mapping software used, and other factors when shooting. |
|---|---|
| Ground Sample Distance(GSD) | (H/36.5) cm/pixel， H means the aircraft altitude relative to shooting scene (unit: m) |
| Data Acquisition Efficiency | Max operating area of approx. 1 km² for a single flight(at an altitude of 182 m, i.e., GSD is approx. 5 cm/pixel, meeting the requirements of the ASPRS Accuracy Standards for Digital Orthophotos Class Ⅲ |
Vision System
| Velocity Range | ≤31 mph(50 kph) at 6.6 ft(2 m) above ground with adequate lighting |
|---|---|
| Altitude Range | 0-33 ft(0 – 10 m) |
| Operating Range | 0-33 ft(0 – 10 m) |
| Obstacle Sensing Range | 2-98 ft(0.7-30 m) |
| FOV | Forward/Rear: 60° (horizontal), ±27° (vertical) Downward: 70° (front and rear), 50° (left and right) |
| Measuring Frequency | Forward/Rear：10 Hz; Downward： 20 Hz |
| Operating Environment | Surfaces with clear patterns and adequate lighting(＞ 15 lux) |
Camera
| Sensor | 1″ CMOS; Effective pixels: 20 M |
|---|---|
| Lens | FOV 84°；8.8 mm / 24 mm(35 mm format equivalent:24 mm)； f/2.8 – f/11, auto focus at 1 m – ∞ |
| ISO Range | Video:100-3200(Auto) 100-6400(Manual)；Photo:100-3200(Auto) 100-12800(Manual) |
| Mechanical Shutter Speed | 8 – 1/2000 s |
| Electronic Shutter Speed | 8 – 1/8000 s |
| Max Image Size | 4864×3648（4:3）； 5472×3648（3:2） |
| Video Recording Modes | H.264，4K：3840×2160 30p |
| Photo Format | JPEG |
| Video Format | MOV |
| Supported File Systems | FAT32（≤ 32 GB）； exFAT（>32 GB） |
| Supported SD Cards | MicroSD, Max Capacity: 128 GB. Class 10 or UHS-1 rating required Write speed≥15 MB/s |
| Operating Temperature Range | 32° to 104° F （0° to 40℃） |
Intelligent Flight Battery(PH4-5870mAh-15.2V)
| Capacity | 5870 mAh |
|---|---|
| Voltage | 15.2 V |
| Battery Type | LiPo 4S |
| Energy | 89.2 Wh |
| Net Weight | 468 g |
| Charging Temperature Range | 14° to 104℉(-10° to 40℃) |
| Max charging Power | 160 W |
Intelligent Battery Charing Hub(WCH2)
| Input Voltage | 17.3 – 26.2 V |
|---|---|
| Output Voltage and Current | 8.7 V，6 A；5 V，2 A |
| Operating Temperature | 41° to 104℉(5° to 40℃) |
GNSS
| Single-Frequency, High-Sensitivity GNSS Module | GPS+BeiDou+Galileo*（Asia)； GPS+GLONASS+Galileo*（other regions） |
|---|---|
| Multi-Frequency Multi-System High-Precision RTK GNSS | Frequency Used： GPS：L1/L2； GLONASS：L1/L2； BeiDou：B1/B2； Galileo*：E1/E5aFirst-Fixed Time：<50 sPositioning Accuracy: Vertical 1.5 cm + 1 ppm（RMS）； Horizontal 1 cm + 1 ppm（RMS） 1 ppm means the error has a 1mm increase for every 1 km of movement from the aircraft. *Available soon |
Gimbal
| Stabilization | 3-axis (tilt, roll, yaw) |
|---|---|
| Pitch | -90° to +30° |
| Max Controllable Angular Speed | 90°/s |
| Angular Vibration Range | ±0.02° |
Infrared
| Obstacle Sensing Range | 0.6-23 ft(0.2 – 7 m) |
|---|---|
| FOV | 70°(Horizontal) ±10°(Vertical) |
| Measuring Frequency | 10 Hz |
| Operating Environment | Surface with diffuse reflection material, and reflectivity＞ 8%（such as wall,trees, humans, etc.) |
Remote Controller
| Operating Frequency | 2.400 GHz-2.483 GHz(Europe,Japan,Korea) 5.725 GHz-5.850 GHz(United States, China) |
|---|---|
| Transmission Power (EIRP) | 2.4 GHz CE / MIC / KCC：<20 dBm5.8 GHz SRRC / FCC：<26 dBm |
| Max Transmission Distance | FCC：4.3 mi(7 km)； SRRC / CE / MIC / KCC：3.1 mi(5 km) (Unobstrcted, free of interference) |
| Power Consumption | 16 W(typical value) |
| Display | 5.5 inch screen, 1920×1080, 1000 cd/m², Android System Memory 4G RAM+16G ROM |
| Operating Temperature Range | 32° to 104° F （0° to 40℃） |
Intelligent Flight Battery Charging Hub(PHANTOM 4 CHARING HUB)
| Voltage | 17.5 V |
|---|---|
| Operating Temperature Range | 41° to 104℉(5° to 40℃) |
| Capacity | 4920 mAh |
| Voltage | 7.6 V |
| Battery Type | LiPo 2S |
| Energy | 37.39 Wh |
| Operating Temperature | -4° to 104℉(-20° to 40℃) |
AC Power Adapter(PH4C160)
| Voltage | 17.4 V |
|---|---|
| Rated Power | 160 W |
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