🚨 Industry Pain Points
Modern unmanned systems operating in complex combat or mission environments often face critical challenges:
- Limited launch flexibility across different operational platforms
- Structural failure risks during high-overload launch conditions
- Dependence on GPS signals for navigation and targeting accuracy
- Inability to maintain coordinated formation flight in dynamic environments
- Reduced mission reliability in GPS-denied or jammed environments
These limitations restrict operational effectiveness in high-intensity and contested scenarios.
⚙ Product Advantages
This system is designed to overcome extreme operational challenges with advanced aerospace-grade capabilities:
- ✔ Supports both ground launch and airborne canister launch systems
- ✔ Withstands up to 50G launch overload for high-stress deployment scenarios
- ✔ Enables coordinated formation flight for multi-platform operations
- ✔ Supports satellite-navigation-based precision strike to fixed coordinates
- ✔ Fully autonomous GPS-free flight using inertial navigation (INS)
- ✔ High structural resilience for harsh launch environments
🚁 Product Applications
This system is suitable for advanced unmanned mission operations, including:
- Tactical UAV formation missions
- Long-range precision strike systems
- Military training and simulation systems
- Border surveillance and reconnaissance operations
- Anti-jamming and GPS-denied mission environments
- Rapid deployment unmanned aerial platforms
⭐ Why Choose Us
- Engineered for extreme launch environments up to 50G
- Dual-mode launch compatibility (ground + airborne canister)
- High-precision navigation in GPS-contested environments
- Stable formation flight control capability
- Proven performance in complex mission scenarios
- Modular integration for different UAV platforms
We provide mission-ready solutions designed for reliability, precision, and operational flexibility in demanding environments.
❓ Frequently Asked Questions (FAQ)
Q1: Can the system operate without GPS?
Yes, it fully supports inertial navigation (INS) for GPS-denied environments.
Q2: What launch methods are supported?
It supports both ground-based and airborne canister launch systems.
Q3: Can it withstand high overload during launch?
Yes, it is designed to withstand up to 50G launch acceleration.
Q4: Does it support coordinated flight?
Yes, it supports formation flight for multi-unit operations.
Q5: Can it perform precision strike missions?
Yes, it supports satellite-navigation-based fixed-coordinate targeting.
| Item | Specification |
|---|---|
| IMU Sensor | 1 |
| GPS Quantity | 1 |
| Power Supply | 8–60V |
| Operating Temperature | -20 to +55 °C |
| Built-in IMU Vibration Isolation | × |
| Built-in RTK | × |
| Built-in Dual-Antenna Direction Finding | × |
| Gimbal (Seeker) Support | √ |
| Engine Support | × |
| Airspeed Measurement Method | Single Pitot Tube (Dynamic Pressure) |
| Power Consumption | < 3W |
| Attitude Accuracy | 1° |
| Heading Accuracy | 2° |
| Gyroscope Measurement Range | ±450 °/s |
| Accelerometer Measurement Range | ±8 g |
| Positioning Accuracy | 2.5 m |
| Velocity Accuracy | 0.1 m/s |
| Airspeed Measurement Range | 0–100 m/s |
| PWM Channels | 14 channels |
| SBUS Input | 1 channel |
| Voltage Monitoring Channels | 2 channels |
| Voltage Monitoring Range | 0–60V (high-voltage module optional) |
| CAN Interface | 1 |
| Serial Ports | 4 × TTL |
| Ethernet | 0 |
| Dimensions | 82 × 62 × 18 mm |
| Weight | 94 g |
