Revision 6d3689c31de5681b972536ebf15f82b4c07fccf5 authored by Gautier Hattenberger on 21 June 2012, 07:39:43 UTC, committed by Gautier Hattenberger on 21 June 2012, 07:47:28 UTC
The mass estimation for the vertical control was not converging after the modification of the range of input thrust from [0,200] to [0, 9600]. The resolution of the estimated value has been adapted to the new range. This code has been tested in flight and maximum values have been checked to prevent overflow, but a cross-check is always welcome.
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| File | Mode | Size |
|---|---|---|
| conf | ||
| data | ||
| debian | ||
| doc | ||
| src | ||
| sw | ||
| tests | ||
| .gitignore | -rw-r--r-- | 3.8 KB |
| AUTHORS | -rw-r--r-- | 1.7 KB |
| BUGS | -rw-r--r-- | 116 bytes |
| COPYING | -rw-r--r-- | 17.6 KB |
| Doxyfile | -rw-r--r-- | 71.5 KB |
| Makefile | -rw-r--r-- | 8.6 KB |
| Makefile.ac | -rw-r--r-- | 6.7 KB |
| Makefile.install | -rw-r--r-- | 8.3 KB |
| README.md | -rw-r--r-- | 2.7 KB |
| githelper.sh | -rwxr-xr-x | 7.4 KB |
| pprz_src_test.sh | -rw-r--r-- | 171 bytes |
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