dji Phantom 4 RTK Посібник із швидкого старту - Сторінка 8

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dji Phantom 4 RTK Посібник із швидкого старту

Specifications

Aircraft
Weight (Battery & Propellers Included)
Max Service Ceiling Above Sea Level
Max Ascent Speed
Max Descent Speed
Max Speed
Max Flight Time
Operating Temperature
Operating Frequency
EIRP
Hover Accuracy Range
Image Position Offset
GNSS
Single-Frequency High-Sensitivity
GNSS
Multi-Frequency Multi-System High-
Precision RTK GNSS
Mapping Functions
Mapping Accuracy**
Ground Sample Distance (GSD)
Acquisition Efficiency
Gimbal
Controllable Range
Vision System
Velocity Range
Altitude Range
Operating Range
Obstacle Sensory Range
Operating Environment
Infrared Sensing System
Obstacle Sensory Range
Operating Environment
Camera
Sensor
Lens
ISO Range
* supported later
** The actual accuracy depends on surrounding lighting and patterns, aircraft altitude, mapping software used, and other factors when
shooting.
1391 g
19685 ft (6000 m)
6 m/s (automatic flight); 5 m/s (manual control)
3 m/s
31 mph (50 kph) (P-mode); 36 mph (58 kph) (A-mode)
Approx. 30 minutes
32° to 104° F (0° to 40° C)
2.400 GHz to 2.483 GHz (Europe, Japan, Korea)
5.725 GHz to 5.850 GHz (United States, China)
2.4 GHz
CE (Europe) / MIC (Japan) / KCC (Korea): < 20 dBm
5.8 GHz
FCC (United States) / SRRC (Mainland China) / NCC (Taiwan, China): < 26 dBm
RTK enabled and functioning properly:
Vertical: ±0.1 m; Horizontal: ±0.1 m
RTK 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)
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.
GPS + BeiDou + Galileo* (Asia); GPS + GLONASS + Galileo* (other regions)
Frequency Used
GPS: L1/L2; GLONASS: L1/L2; BeiDou: B1/B2; Galileo*: E1/E5
First-Fixed Time: < 50 s
Positioning Accuracy: Vertical 1.5 cm + 1 ppm (RMS); Horizontal 1 cm + 1 ppm (RMS).
1 ppm indicates error with a 1 mm increase over 1 km of movement.
Velocity Accuracy: 0.03 m/s
Mapping accuracy meets the requirements of the ASPRS Accuracy Standards for Digital
Orthophotos Class III.
(H/36.5) cm/pixel, H indicates the aircraft altitude relative to the shooting scene (unit: m)
Max operating area of approx. 1 km
approx. 5 cm/pixel, meeting the requirements of the ASPRS Accuracy Standards for Digital
Orthophotos Class III).
Pitch: -90° to +30°
≤ 31 mph (50 kph) at 6.6 ft (2 m) above ground with adequate lighting
0 - 33 ft (0 - 10 m)
0 - 33 ft (0 - 10 m)
2 - 98 ft (0.7 - 30 m)
Surfaces with clear patterns and adequate lighting (> 15 lux)
0.6 - 23 ft (0.2 - 7 m)
Surface with diffuse reflection material, and reflectivity > 8% (such as wall, trees, humans, etc.)
1'' CMOS; Effective pixels: 20M
FOV (Field of View) 84°, 8.8 mm (35 mm format equivalent: 24 mm), f/2.8 - f/11, auto focus
at 1 m - ∞
Video: 100 - 3200 (Auto), 100 - 6400 (Manual); Photo: 100 - 3200 (Auto), 100 - 12800 (Manual)
for a single flight (at an altitude of 182 m, i.e., GSD is
2
Y
X
Z
131 mm
72 mm