Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4179 d 22 h /branches/dongfang_FC_rewrite/  
2160 4365 d 9 h /branches/dongfang_FC_rewrite/  
2052 4475 d 19 h /branches/dongfang_FC_rewrite/  
2051 4477 d 9 h /branches/dongfang_FC_rewrite/  
2049 4478 d 9 h /branches/dongfang_FC_rewrite/  
2048 4479 d 8 h /branches/dongfang_FC_rewrite/  
2041 4484 d 8 h /branches/dongfang_FC_rewrite/  
2035 4491 d 8 h /branches/dongfang_FC_rewrite/  
1980 4630 d 11 h /branches/dongfang_FC_rewrite/  
1874 4817 d 11 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 4818 d 19 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4821 d 1 h /branches/dongfang_FC_rewrite/  
1805 4924 d 19 h /branches/dongfang_FC_rewrite/  
1775 4968 d 10 h /branches/dongfang_FC_rewrite/  
1645 5131 d 11 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 5146 d 12 h dongfang /branches/dongfang_FC_rewrite/ Initial import.