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Volumn , Issue , 2011, Pages 5166-5172

Design of a flexible high performance quadcopter platform breaking the MAV endurance record with laser power beaming

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL STRUCTURE; FLIGHT CONTROL; FLIGHT TIME; LASER POWER; LASER POWER BEAMING; MATLAB /SIMULINK; MECHANICAL DESIGN;

EID: 84455167471     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/IROS.2011.6048336     Document Type: Conference Paper
Times cited : (94)

References (11)
  • 2
  • 3
    • 84855585105 scopus 로고    scopus 로고
    • Design of an Ultra-Lightweight Autonomous Solar Airplane for Continuous Flight
    • Zurich, Switzerland, December
    • A. Noth and R. Siegwart, "Design of an Ultra-Lightweight Autonomous Solar Airplane for Continuous Flight," Aircraft and Spacecraft Systems Design Lecture Notes, Zurich, Switzerland, December 2006, http://www.asl.ethz. ch/research/asl/skysailor/Design.
    • (2006) Aircraft and Spacecraft Systems Design Lecture Notes
    • Noth, A.1    Siegwart, R.2
  • 8
    • 84855584626 scopus 로고    scopus 로고
    • website
    • Ascending Technologies GmbH, website, http://www.asctec.de.
  • 11
    • 19644368255 scopus 로고    scopus 로고
    • Dynamic Inversion Based Control Concept with Application to an Unmanned Aerial Vehicle
    • August
    • F. Holzapfel and G. Sachs, "Dynamic Inversion Based Control Concept with Application to an Unmanned Aerial Vehicle," in AIAA Guidance, Navigation, and Control, August 2004.
    • (2004) AIAA Guidance, Navigation, and Control
    • Holzapfel, F.1    Sachs, G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.