File:Computer simulation of artillery rocket trajectory improvement using fixed canards trajectory correction fuze.jpg
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Summary
| Description |
English: Computer simulation of artillery rocket trajectory improvement using fixed canards trajectory correction fuze.
The simulation results for the control activation time of 90 seconds. Results show that larger correction ability is obtained when control is activated earlier in the flight (90 s) while smaller correction ability is obtained when control is activated later (100 s) in the flight. For example, when control is activated at 90 s it can achieved ‘range’ control authority from 32 km to 48 km, whereas ‘drift’ control authority of 12 km can be achieved on both sides of the ‘drift’ axis. |
| Date | |
| Source | "Range and Accuracy Improvement of Artillery Rocket Using Fixed Canards Trajectory Correction Fuze" Aerospace 9, no. 1: 32. 2022 https://doi.org/10.3390/aerospace9010032 |
| Author | Raza, Ali, and Hua Wang |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 07:40, 10 April 2022 | | 2,023 × 1,510 (290 KB) | Technophant | Uploaded a work by Raza, Ali, and Hua Wang from "Range and Accuracy Improvement of Artillery Rocket Using Fixed Canards Trajectory Correction Fuze" Aerospace 9, no. 1: 32. 2022 https://doi.org/10.3390/aerospace9010032 with UploadWizard |
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