지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2012.10
- 수록면
- 1,738 - 1,741 (4page)
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초록· 키워드
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Flight test results of flight control performance of Smart UAV were described. Flight test in airplane mode was performed by internal pilot using automatic functions including auto take-off and landing, speed/altitude/heading hold as well as a point navigation and a preprogram mode. It reached to the designed maximum speed at operational altitude. The rotor speed in airplane mode was reduced to 82% from 98% RPM in order to increase rotor efficiency with reducing Mach number at tip of rotors. Rotor governor was designed to maintain dual variable rotor speed in the flight control law. The performance of flight control including speed, altitude, heading error as well as damping and frequency were evaluated in all flight envelope in the airplane mode. These control laws were modified to meet the design requirement of Smart UAV.
This paper presents the flight test result of airplane mode of Smart UAV. Detailed test plan and the flight control performance were also described.
This paper presents the flight test result of airplane mode of Smart UAV. Detailed test plan and the flight control performance were also described.
목차
Abstract
1. INTRODUCTION
2. TEST PROCEDURES
3. FLIGHT TEST RESULTS
4. CONCULUSIONS
REFERENCES
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