Identification of Saras flight stability and control characteristics

Singh, Jatinder and Kumar, Vineet and Basappa, - and Panda, GK (2008) Identification of Saras flight stability and control characteristics. In: Proceedings of the International Conference on Aerospace Science and Technology (INCAST 2008-116), 26-28 Jun 2008, Bangalore, India.

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    Abstract

    Longitudinal stability and control characteristics and the neutral point of Saras aircraft are estimated from flight test data by applying classical and parameter identification techniques. The accuracy of the nose boom and the side-mounted angle-of-attack vanes is assessed using steady-state level flight data. The angle-of-attack accuracy is also assessed by applying flight path reconstruction techniques to flight data from short period pitch stick maneuvers. Results from the classical and parameter identification techniques are compared with the design data from wind tunnel tests.

    Item Type: Conference or Workshop Item (Paper)
    Additional Information: Copyright for this article belongs to National Aerospace Laboratories
    Uncontrolled Keywords: Saras aircraft;Flight stability;Nose boom
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Flight Mechanics and Control Division, Centre for Civil Aircraft Design and Development, Flight Mechanics and Control Division, Centre for Civil Aircraft Design and Development
    Depositing User: Ms. Alphones Mary
    Date Deposited: 23 Mar 2009
    Last Modified: 17 Jun 2010 14:49
    URI: http://nal-ir.nal.res.in/id/eprint/5025

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