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
- 2011.10
- 수록면
- 877 - 880 (4page)
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초록· 키워드
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Flight test results of flying qualities for Helicopter mode of Smart UAV are described. Flight test items in helicopter mode include manual and automatic stick control as well as hold and navigation flight including automatic take off and landing. One of the main purposes of helicopter mode flight test is to evaluate the handling qualities in low speed region where nacelle angles are greater than 80 deg. Rotor speed was controlled by the rotor governor without electric engine control after engine start. Position holding GPS stick mode and pitch/roll attitude SCAS (Stability and Control Augmentation System) showed good handling qualities performance during helicopter flight test. These control laws are also the basis both of conversion mode and airplane mode. All flight test described in this paper were controlled by external pilot (EP) using augmented GPS stick mode which comprise of 3 axis speed command and yaw rate command as well as position/heading hold at a neutral stick position. This paper presents the flight test result of flying qualities for helicopter mode of Smart UAV.
목차
Abstract
1. INTRODUCTION
2. TEST PROCEDURES
3. Flight TEST RESULTS
4. CONCLUSION
REFERENCES
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UCI(KEPA) : I410-ECN-0101-2014-569-000913756