Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4267 d 4 h /branches/dongfang_FC_rewrite/  
2160 4452 d 14 h /branches/dongfang_FC_rewrite/  
2052 4563 d 1 h /branches/dongfang_FC_rewrite/  
2051 4564 d 15 h /branches/dongfang_FC_rewrite/  
2049 4565 d 15 h /branches/dongfang_FC_rewrite/  
2048 4566 d 14 h /branches/dongfang_FC_rewrite/  
2041 4571 d 13 h /branches/dongfang_FC_rewrite/  
2035 4578 d 14 h /branches/dongfang_FC_rewrite/  
1980 4717 d 17 h /branches/dongfang_FC_rewrite/  
1874 4904 d 16 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 4906 d 0 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4908 d 7 h /branches/dongfang_FC_rewrite/  
1805 5012 d 1 h /branches/dongfang_FC_rewrite/  
1775 5055 d 16 h /branches/dongfang_FC_rewrite/  
1645 5218 d 17 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 5233 d 17 h dongfang /branches/dongfang_FC_rewrite/ Initial import.