Advanced Parameter Estimation Studies of TEJAS Aircraft from High Angle-of-Attack Flight Data

Jatinder, Singh and Parameswaran, V (2004) Advanced Parameter Estimation Studies of TEJAS Aircraft from High Angle-of-Attack Flight Data. Technical Report. NAL, Bangalore.

Full text available as:
[img] PDF
Download (51Kb)

    Abstract

    This Document Is A Project Proposal To Carry Out Aerodynamic Parameter Estimation Of LCA From High Angle-Of-Attack Flight Test Data . Various Activities Like The Coefficient Level Matching,Analysis Of Large Amplitude Maneuver Data And Global Model Identification Are Planned .A Brief Description Of These Tasks Is Highlighted In The Proposal.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Parameter Estimation; Stability And Control Derivatives; Flight Data; Aerodynamic Modeling; Global Modeling; Nonlinear Methods
    Subjects: ASTRONAUTICS > Astronautics (General)
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 06 Aug 2012 10:34
    Last Modified: 06 Aug 2012 10:34
    URI: http://nal-ir.nal.res.in/id/eprint/10708

    Actions (login required)

    View Item