| Autor: |
CHENG Zhen-xuan, QI Zai-kang, LIN De-fu, FAN Jun-fang |
| Předmět: |
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| Zdroj: |
Transactions of Beijing Institute of Technology; 2009, Vol. 29 Issue 4, p283-285, 3p, 1 Diagram, 5 Graphs |
| Abstrakt: |
To obtain pivotal aerodynamic parameters when studying missiles, a new method of aerodynamic parameter identification with dual-accelerometer is proposed, its hardware configuration and the detailed process are presented. This method can identify the weathercock frequency, angle of attack, over loading, lift coefficient, etc. Actual flight test showed that it could obtain some important aerodynamic parameters according to the use with dual-accelerometer. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Supplemental Index |
| Externí odkaz: |
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