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|Title: ||On the development of parameterized linear analytical longitudinal airship models|
|Authors: ||Kulczycki, Eric A.|
Johnson, Joseph R.
Bayard, David S.
Quadrelli, Marco B.
|Issue Date: ||18-Aug-2008 |
|Publisher: ||Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2008.|
|Citation: ||AIAA AIAA Guidance, Navigation and Control Conference and Exhibit 2008, Honolulu, Hawaii, August 18, 2008.|
|Abstract: ||In order to explore Titan, a moon of Saturn, airships must be able to traverse the atmosphere autonomously. To achieve this, an accurate model and accurate control of the vehicle must be developed so that it is understood how the airship will react to specific sets of control inputs. This paper explains how longitudinal aircraft stability derivatives can be used with airship parameters to create a linear model of the airship solely by combining geometric and aerodynamic airship data. This method does not require system identification of the vehicle. All of the required data can be derived from computational fluid dynamics and wind tunnel testing. This alternate method of developing dynamic airship models will reduce time and cost. Results are compared to other stable airship dynamic models to validate the methods. Future work will address a lateral airship model using the same methods.|
|Appears in Collections:||JPL TRS 1992+|
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