Subversion Repositories FlightCtrl

Rev

Show changed files | Details | Compare with Previous | Blame | RSS feed

Filtering Options

Rev Age Author Path Log message Diff
2189 4369 d 6 h /branches/dongfang_FC_rewrite/  
2160 4554 d 16 h /branches/dongfang_FC_rewrite/  
2052 4665 d 3 h /branches/dongfang_FC_rewrite/  
2051 4666 d 17 h /branches/dongfang_FC_rewrite/  
2049 4667 d 16 h /branches/dongfang_FC_rewrite/  
2048 4668 d 15 h /branches/dongfang_FC_rewrite/  
2041 4673 d 15 h /branches/dongfang_FC_rewrite/  
2035 4680 d 16 h /branches/dongfang_FC_rewrite/  
1980 4819 d 18 h /branches/dongfang_FC_rewrite/  
1874 5006 d 18 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 5008 d 2 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 5010 d 8 h /branches/dongfang_FC_rewrite/  
1805 5114 d 2 h /branches/dongfang_FC_rewrite/  
1775 5157 d 17 h /branches/dongfang_FC_rewrite/  
1645 5320 d 19 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 5335 d 19 h dongfang /branches/dongfang_FC_rewrite/ Initial import.