Exploring some key problems in modeling a stratospheric airship

Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

Volumn 25, Issue 3, 2007, Pages 383-387

  Chen, Lan ^a   An, Jinwen ^a   Yang, Changwei ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Additional mass; Moment of inertia; Six degree of freedom dynamic model; Stratospheric airship

Indexed keywords

BUOYANCY; COMPUTER PROGRAM LISTINGS; COMPUTER SIMULATION; DYNAMIC MODELS; GRAVITATION; MATHEMATICAL MODELS;

ADDITIONAL MASS; INERTIA MOMENT; SIX DEGREE FREEDOM DYNAMIC MODEL; STRATOSPHERIC AIRSHIP;

AIRSHIPS;

EID: 34547630362     PISSN: 10002758     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (7)

1. Masahiko Onda. Design Considerations on Stratospheric LTA Platform. 13th AIAA Lighter-Than-Air Systems Technology Conference, Norfolk, VA, 1999, 204-209
2. Ryu M, Mikio S. R&D on Telecom and Broadcasting System Using High Altitude Platforms Conducted by CTL/TAO. The 3rd Stratospheric Platform Systems Workshop, Tokyo, Japan, 2001, 21-29
3. Sergio B V G, Josue Jr G Ramos. Airship Dynamic Modeling for Autonomous Operation. Proceedings of the IEEE International Conference on Robotics and Automation, Leuven, Belgium, 1998, 3462-3467
4. Masaaki Sano, Keiji Komatsu, et al. Airship Shaped Balloon Test Flight to the Stratosphere. AIAA's 3rd Annual Aviation Technology, Integration, and Operations (ATIO) Tech, Denver, Colorado, 2003, 1-6
5. Steiner Volker. How to Improve the Performance of an LTA Vehicle (Balloon or Airship). 12th AIAA Lighter-than-Air Systems Technology Conference, San Francisco, CA, 1997, 211-221