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dongfang_FC_rewrite
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attitude.h
@ 1756
- Rev 2189
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2189
4345 d 1 h
/branches/dongfang_FC_rewrite/
2160
4530 d 12 h
/branches/dongfang_FC_rewrite/
2052
4640 d 22 h
/branches/dongfang_FC_rewrite/
2051
4642 d 12 h
/branches/dongfang_FC_rewrite/
2049
4643 d 12 h
/branches/dongfang_FC_rewrite/
2048
4644 d 11 h
/branches/dongfang_FC_rewrite/
2041
4649 d 10 h
/branches/dongfang_FC_rewrite/
2035
4656 d 11 h
/branches/dongfang_FC_rewrite/
1980
4795 d 14 h
/branches/dongfang_FC_rewrite/
1874
4982 d 14 h
/branches/dongfang_FC_rewrite/
Gyro factor of 4 removed.
Sign extension experiment
Mixer matrix execution now solved: No overflows and only 1 32 bit division (implemented with right shifting w sign extension)
Axis coupling disabled by default (until it starts working well...)
1872
4983 d 22 h
/branches/dongfang_FC_rewrite/
Performance problems fixed.
1869
4986 d 4 h
/branches/dongfang_FC_rewrite/
1805
5089 d 22 h
/branches/dongfang_FC_rewrite/
1775
5133 d 13 h
/branches/dongfang_FC_rewrite/
1645
5296 d 14 h
/branches/dongfang_FC_rewrite/
Gyro measurement, gypo signal processing, attitude calculation and flight calculation were almost identical for pitch and roll. Therefore, arrays are now used for pitch and roll stuff + common code for both.
Gyro saturation prevention added.
Filtering and other processing of gyro signals modified.
1612
5311 d 14 h
dongfang
/branches/dongfang_FC_rewrite/
Initial import.