Algorithms for aircraft trim analysis on ground 13; AIAA-96-350513;

Pashilkar, AA (1996) Algorithms for aircraft trim analysis on ground 13; AIAA-96-350513;. In: AIAA flight simulation technologies conference.

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    Abstract

    In the analysis of aircraft dynamics far up and13; away flight, the general practice consists of trimming13; the aircraft for a specific maneuvers at a specified13; Altitude and Mach number. In this paper conditions for13; Quasi-steady equilibrium are motivated for aircraft13; dynamics in the ground roll phase. Algorithms for13; implementation of these conditions are also described.13; By use of these algorithms, the locus of trim points is13; obtained for a comprehensive take-off maneuvers of a13; delta wing aircraft beginning with ground roll,13; followed by rotation and ending in lift-off. This result13; is compared with approximate calculations wherein the13; landing gear states are ignored and linear13; aerodynamics is assumed. The exact result is also13; compared with the simulation of the take-off13; maneuvers in a pilot in the loop simulator.13;

    Item Type: Conference or Workshop Item (Paper)
    Uncontrolled Keywords: Algorithms;Aircraft wings
    Subjects: AERONAUTICS > Avionics & Aircraft Instrumentation
    Division/Department: Flight Mechanics and Control Division
    Depositing User: Mrs Manoranjitha M D
    Date Deposited: 23 Feb 2006
    Last Modified: 24 May 2010 09:40
    URI: http://nal-ir.nal.res.in/id/eprint/1061

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