Instrument Modeling for Aerodynamic Coefficient Identification from Flight Test Data
- 1 May 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 3 (3) , 275-279
- https://doi.org/10.2514/3.55984
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Effects of unsymmetrical stability derivative characteristics on re-entry vehicle transient angular motionJournal of Spacecraft and Rockets, 1976
- Square Root Variable Metric Method for Function MinimizationAIAA Journal, 1975
- A method for extracting aerodynamic coefficients from free-flight dataAIAA Journal, 1970