Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4322 d 1 h /branches/dongfang_FC_rewrite/  
2160 4507 d 12 h /branches/dongfang_FC_rewrite/  
2052 4617 d 22 h /branches/dongfang_FC_rewrite/  
2051 4619 d 12 h /branches/dongfang_FC_rewrite/  
2049 4620 d 12 h /branches/dongfang_FC_rewrite/  
2048 4621 d 11 h /branches/dongfang_FC_rewrite/  
2041 4626 d 11 h /branches/dongfang_FC_rewrite/  
2035 4633 d 11 h /branches/dongfang_FC_rewrite/  
1980 4772 d 14 h /branches/dongfang_FC_rewrite/  
1874 4959 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 4960 d 22 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4963 d 4 h /branches/dongfang_FC_rewrite/  
1805 5066 d 22 h /branches/dongfang_FC_rewrite/  
1775 5110 d 13 h /branches/dongfang_FC_rewrite/  
1645 5273 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 5288 d 15 h dongfang /branches/dongfang_FC_rewrite/ Initial import.