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학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
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연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 저널정보
- 한국항공우주학회 한국항공우주학회 학술발표회 초록집 Proceedings of KSAS-JSASS Joint International Symposium on Aerospace Engineering
- 발행연도
- 2008.11
- 수록면
- 504 - 507 (4page)
이용수
이 논문의 연구 히스토리 (3)
2008
Automatic Take-off and Landing of the Small Scaled Tilt Rotor UAV based on Single GPS/INS
Youngshin Kang
,
Bumjin Pa
,
k
외 4명
한국항공우주학회 학술발표회 초록집
2008.11
학술대회자료
Flight Test Results of Automatic Tilt Control for Small Scaled Tilt Rotor Aircraft
Youngshin Kang
,
Bumjin Pa
,
k
외 3명
제어로봇시스템학회 국제학술대회 논문집
2008.10
학술대회자료
- 이 논문의 후속연구가 궁금하신가요?
- 연관 학술논문 또는 학술발표를 통해 보다 발전된 연구결과를 확인하실 수 있습니다.
- 이 논문의 연구 히스토리 확인하기
초록· 키워드
오류제보하기
A small scaled night model of the tilt rotor aircraft for the Smart UAV Program at KARl (Korea Aerospace Research Institute) has been developed and tested.
The night test of automatic take off and landing of the small scaled model was performed as the final test phase. The control laws for automatic take off and landing was designed based on a single GPS/INS. Since the error of single GPS/INS was nut negligible so that an automatic landing algorithm with the sensor error was considered. The night test procedure for the automatic take off and landing was considered to prove the performance of a single GPS/INS sensor and flight characteristics of small tilt rotor aircraft The test procedure was scheduled as an automatic take off, a climb with acceleration while point turn, an change of the turn point. a descent with deceleration in point turn, an automatic approach to hover, and an automatic landing. All of the control inputs were made by an internal pilot (IP).
The night test results and the detailed procedure of the night test for the automatic takeoff and landing of the small scaled lilt rotor aircraft is presented in this paper.
The night test of automatic take off and landing of the small scaled model was performed as the final test phase. The control laws for automatic take off and landing was designed based on a single GPS/INS. Since the error of single GPS/INS was nut negligible so that an automatic landing algorithm with the sensor error was considered. The night test procedure for the automatic take off and landing was considered to prove the performance of a single GPS/INS sensor and flight characteristics of small tilt rotor aircraft The test procedure was scheduled as an automatic take off, a climb with acceleration while point turn, an change of the turn point. a descent with deceleration in point turn, an automatic approach to hover, and an automatic landing. All of the control inputs were made by an internal pilot (IP).
The night test results and the detailed procedure of the night test for the automatic takeoff and landing of the small scaled lilt rotor aircraft is presented in this paper.
목차
Abstract
1. INTRODUCTION
2. FLIGHT TEST PROCEDURE
3. SENSOR ACCURACY TEST
4. FLIGHT TEST RESULTS
5. CONCLUSION
ACKNOWLEDGMENT
REFERENCES
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