Mohan Ram, VS and Raol, JR and Jagadeesh, M (1987) Flight Test Specification for Missile Parameter Identification. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
This document describes a -method of selecting and specifying a suitable test input signal for aerodynamic parameter identification of a missile with the autopilot in the loop, Recommendations for implementation of a parameter identification flight test program in the altitude range of 18 km to 5 km using a chain of doublet input signals are proposed in this document
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Flight Test specification, Missile Parameter Identification |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 06 Jul 2012 16:10 |
| Last Modified: | 06 Jul 2012 16:10 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10525 |
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