Srinathkumar, S and Padma, Maduranath 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 |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 07 Mar 2006 |
| Last Modified: | 24 May 2010 09:40 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1071 |
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