Product brief introduction
This product supports fixed wing, rotor wing, composite wing and other types of UAV. Support full-automatic flight, stabilization flight and airline task switching in flight, adopt the self-adapting flight control navigation algorithm and effective emergency processing algorithm, realize high-precision attitude trajectory control and flexible airline edit function, have the voyage protection, flame-out protection, GPS satellite losing protection, and other emergency response mechanisms. Carry dual-redundancy GNSS integrated navigation system, can provide reliable course pitching and rolling attitude information, longitude, latitude, and altitude locating information, and 3d acceleration and angular velocity, and other inertial measurement information. At the same time, the product supports ground simulation flight and can simulate UAV flight training.
Product feature
Support many types of UAV, such as fixed wing, rotor wing, and composite wing, etc.
Support multiple full-automatic airplane mode (constant navigation course mode, multipleair linesswitching mode, waypoint tracking mode, autonomous course reversal mode, and spiral model, etc.)
Customizable ability of emergency management (voyage protection, flame-out protection, electronic fence protection, and GPS satellite losing protection, etc.); can support scheme for emergent treatment configured by users;
In-built 4G memorizer, can completely record 4-8-hour flight data
Heterogeneous dual-redundancy inertial element
Dual-redundancy GNSS multi-mode automatic shift
Support various flight emulation mode, have multiple emulation modes, such as PIL, SIL and HIL, and can carry out daily simulated training for UAV operating personnel;
Power supply design with high reliability of redundancy
Performance index
System performance index
|
Parameters |
Numerical value |
Remarks |
|
Starting time |
5 |
|
|
Update frequency (Hz) |
50，100 |
|
|
Operating temperature (℃) |
|
|
|
Horizontal position precision (m) |
5 |
GNSS single-point, RMS |
|
0.5 |
GNSS RTK，RMS |
|
|
Positional accuracy of elevation (m) |
10 |
GNSS single-point, RMS |
|
1 |
GNSS RTK，RMS |
|
|
Horizontal velocity and precision (m/s) |
0.3 |
GNSS single-point, RMS |
|
0.1 |
GNSS RTK，RMS |
|
|
Vertical velocity and precision (m/s) |
0.5 |
GNSS single-point, RMS |
|
0.2 |
GNSS RTK，RMS |
|
|
Horizontal attitude (°) |
0.6 |
RMS, pitching and rolling |
|
3 |
Receiver is losing lock (<2min) |
|
|
Heading attitude (°) |
2 |
RMS and GNSS have no directional information |
|
0.8 |
RMS and GNSS have directional information |
|
|
120°/h*△T |
Receiver is losing lock and magnetism can't be used |
Physical property
Physical property of system
|
Items |
Indexes |
|
|
Processing capacity |
Operational capability |
Support single and double precision floating point arithmetic |
|
Operational digit |
32 digits |
|
|
Hardware interface |
RS422 |
2-way |
|
RS232/RS422 reuse |
3-way |
|
|
S.BUS (input and output) |
Single way |
|
|
CAN |
2-way |
|
|
PWM |
12-way |
|
|
IO |
12-way |
|
|
USB |
Single way |
|
|
SWD |
Single way |
|
|
Storage |
Capacity |
≮4G |
|
Operating environment |
Operating temperature |
-40℃～+55℃ |
|
Vibration |
9.5g,15Hz～2000Hz |
|
|
Impact |
10g, half-wave sine |
|
|
Electricity |
Supply voltage |
6~16V |
|
Power consumption |
≤14W |
|
|
Structure |
Single-board size |
10×10cm(a) |
Flight control navigation system product
