Earticle

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

키워드

저자

• Asif Sajjad Khan Anjum Salman Afghani [ R & D Department of Engineering Sciences Army Public College of Management and Sciences, Rawalpindi, Pakistan ]
• Mati-ur-Rehman [ R & D Department of Engineering Sciences Army Public College of Management and Sciences, Rawalpindi, Pakistan ]
• Muhammad Safwan Yaseen Khan [ R & D Department of Engineering Sciences Army Public College of Management and Sciences, Rawalpindi, Pakistan ]
• Muhammad Arslan [ R & D Department of Engineering Sciences Army Public College of Management and Sciences, Rawalpindi, Pakistan ]

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  International Journal of Advanced Science and Technology

• 간기

  월간

• pISSN

  2005-4238

• 수록기간

  2008~2016

• 십진분류

  KDC 505 DDC 605