UAV dogfighter
UAV
UAV dogfighter is a high-maneuverability interception UAV system specially designed to counter air threats. Through high-precision optical guidance and real- dynamic tracking technology, it carries out directed collision strikes on enemy UAVs, forcing them to lose control or crash by physical contact.The system integrates GPS command modification and machine vision guidance, and can still stably lock the target and complete the interception task through high-speed penetration maneuvering, in complex electromagnetic environment or low visibility conditions.
Core advantages and technical characteristics
1. Composite guidance for precise interception
-Adopted a multimodal guidance system (optical imaging GPS positioning), significantly improving the capture probability and strike accuracy of low-altitude slow-speed.
2. Active hard kill mode
-Distinguished from traditional soft-kill means (such as signal jamming or net throwing), it directly destroys the target structure through **kinetic impact** especially suitable for high-threat aircraft with anti-electronic jamming capability.
3. Modular rapid deployment
-Support military defense (no-fly zone on the battlefield), critical facility protection (power station, airport), and large-scale event security, etc. with all-weather emergency response capability.
1 | Size (expanded, excluding blades) | 380*400*200mm ( L*W*H ) | ||||
2 | Diagonal motor axle spacing | 550mm | ||||
3 | Unladen weight (including two batteries) | 3.3kg | ||||
4 |
Maximum wind speed | 12 m/s (level six wind) The maximum tolerable wind speed during take-off and landing phases is 10 m/s | ||||
5 | Maximum flight time [1] | 15 minutes (empty route flight) | ||||
6 | Maximum take-off and landing altitude | 4600 meters | ||||
7 | IP protection level[2] | IP54 | ||||
8 | Practical ceiling | 5km | ||||
9 | Landing and take-off method | Rotor take-off and landing | ||||
10 |
Wind resistance | Normal operation at level six wind; no damage at level seven wind. | ||||
11 | control distance | 10km | ||||
12 | Reliability index | MTBF>1000h;MTTR<1h | ||||
13 | Image distance | transmission | communication | 10km | ||
14 | Image transmission interface | Network port; serial port (select one of TTL 232 422) | ||||
15 | Steering motor power plug | Double-circuit plug-in connector | ||||
16 | Flight mode | Pre-set trajectory and real-time control of two flight modes | ||||
17 |
Security features | Automatic protection, protection | return, low broken | voltage propeller | ||
18 | Anti-interference protection measures | have; meet the requirements | ||||
19 | Power interface for load | have; meet the requirements | ||||
20 | Payload mounting structure; | have; meet the requirements | ||||
*Annotation
[1] Maximum flight time and load flight time are tested under laboratory conditions (in zero altitude and no wind), for reference only.
[2] Protective capabilities are not permanent and may decrease due to aging wear caused by long-term use.
[3] The battery life is measured under experimental conditions and is for reference only.
[4] The maximum communication distance is measured in an ideal environment (rural open field, open farmland, etc.) for reference only.

