Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4342 d 1 h /branches/dongfang_FC_rewrite/  
2160 4527 d 11 h /branches/dongfang_FC_rewrite/  
2052 4637 d 22 h /branches/dongfang_FC_rewrite/  
2051 4639 d 12 h /branches/dongfang_FC_rewrite/  
2049 4640 d 12 h /branches/dongfang_FC_rewrite/  
2048 4641 d 11 h /branches/dongfang_FC_rewrite/  
2041 4646 d 10 h /branches/dongfang_FC_rewrite/  
2035 4653 d 11 h /branches/dongfang_FC_rewrite/  
1980 4792 d 14 h /branches/dongfang_FC_rewrite/  
1874 4979 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 4980 d 22 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4983 d 4 h /branches/dongfang_FC_rewrite/  
1805 5086 d 22 h /branches/dongfang_FC_rewrite/  
1775 5130 d 13 h /branches/dongfang_FC_rewrite/  
1645 5293 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 5308 d 14 h dongfang /branches/dongfang_FC_rewrite/ Initial import.