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초록
영어
In this paper we have discussed the development of a new approach for small low cost helicopter based UAV in which independency of control system is achieved and other features like power enhancement, development, flight of helicopter at fix altitude of highly cost effective, autonomous reconnaissance UAV, suitable for safe flights in close environments . Our approach is focused on development of reliable flight control system in which constituent subsystem are independent of each other. The constituent subsystems being, Altitude Control Subsystem Spin Lock Subsystem Horizontal Drift Control Subsystem Auto Pilot, Helicopter, UAV, Independent Control Systems, Fix Altitude, Cost Effective UAV
목차
Abstract
1. Introduction
2. Development of the Design
3. Existing Control System for Helicopter Type uav
3.1. Features
4. Design Modification
4.1. Modified Assembly
4.2. Increase Payload Capacity
5. The Independent Sub-Systems of our Design
5.1. Altitude Control Sub System
5.2. Rotation Lock Sub System
6. Horizontal Drift Control Subsystem
7. Future Work
Acknowledgments
References
1. Introduction
2. Development of the Design
3. Existing Control System for Helicopter Type uav
3.1. Features
4. Design Modification
4.1. Modified Assembly
4.2. Increase Payload Capacity
5. The Independent Sub-Systems of our Design
5.1. Altitude Control Sub System
5.2. Rotation Lock Sub System
6. Horizontal Drift Control Subsystem
7. Future Work
Acknowledgments
References
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