Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4341 d 6 h /branches/dongfang_FC_rewrite/  
2160 4526 d 17 h /branches/dongfang_FC_rewrite/  
2052 4637 d 3 h /branches/dongfang_FC_rewrite/  
2051 4638 d 17 h /branches/dongfang_FC_rewrite/  
2049 4639 d 17 h /branches/dongfang_FC_rewrite/  
2048 4640 d 16 h /branches/dongfang_FC_rewrite/  
2041 4645 d 15 h /branches/dongfang_FC_rewrite/  
2035 4652 d 16 h /branches/dongfang_FC_rewrite/  
1980 4791 d 19 h /branches/dongfang_FC_rewrite/  
1874 4978 d 19 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 4980 d 3 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4982 d 9 h /branches/dongfang_FC_rewrite/  
1805 5086 d 3 h /branches/dongfang_FC_rewrite/  
1775 5129 d 18 h /branches/dongfang_FC_rewrite/  
1645 5292 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 5307 d 19 h dongfang /branches/dongfang_FC_rewrite/ Initial import.