Estimation of neutral and maneuver points of aircraft by dynamic maneuvers AIAA-93-3620

Srinathkumar, S and Padma, Madhuranath and Girija, G (1993) Estimation of neutral and maneuver points of aircraft by dynamic maneuvers AIAA-93-3620. In: AIAA atmospheric flight mechanics conference.

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Abstract

A new flight test technique, based on13; aircraft parameter estimation methods, is13; proposed to simultaneously determine the neutral13; and maneuver point of aircraft. The new13; procedure is derived by relating the neutral point13; and maneuver point of an aircraft to key short13; period parameters Ma and short period natural13; frequency w,' respectively. The new flight test13; method results in substantial savings in flight test13; time compared to conventional methods. The13; method is more accurate since only inertial sensor13; data (pitch rate and normal acceleration) is used13; in the estimation procedure.

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Aircraft maneuver;flight test method;flight test technique
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User: Users 15 not found.
Date Deposited: 07 Mar 2006
Last Modified: 24 Aug 2015 09:46
URI: http://nal-ir.nal.res.in/id/eprint/1071

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