Technical Description
This invention relates to a micro aerial vehicle (MAV) with an integrated actuator system enabling flapping, roll, and sweep wing motions. The design uses a slider-based mechanism to achieve coordinated multi-axis control for improved maneuverability and flight performance.
Problems Addressed
- Complex Linkage Kinematics
- Inefficient Structural Design
- Lacks Operational Reliability
- Bulky Control Systems
- Frequent Structural Failures
- Excessive Motor Stress
Tech Features
- Enhanced Flapping Mechanism
- Efficient Multi-Actuator Control
- Simplified Slider-Piston Assembly
- Optimized Sweep Motion
- Robust Fuselage Integration
- Precision Roll Actuation
Target Audience
- Defense and Surveillance Sectors
- Logistics and Delivery Industries
- Environmental Monitoring Agencies
- Research & Development
Tech ID: P04-1969 TRL 6 Patent Status: Granted Available For Exclusive and Non-exclusive License
