Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4205 d 10 h /branches/dongfang_FC_rewrite/  
2160 4390 d 21 h /branches/dongfang_FC_rewrite/  
2052 4501 d 7 h /branches/dongfang_FC_rewrite/  
2051 4502 d 21 h /branches/dongfang_FC_rewrite/  
2049 4503 d 21 h /branches/dongfang_FC_rewrite/  
2048 4504 d 20 h /branches/dongfang_FC_rewrite/  
2041 4509 d 20 h /branches/dongfang_FC_rewrite/  
2035 4516 d 20 h /branches/dongfang_FC_rewrite/  
1980 4655 d 23 h /branches/dongfang_FC_rewrite/  
1874 4842 d 23 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 4844 d 7 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4846 d 13 h /branches/dongfang_FC_rewrite/  
1805 4950 d 7 h /branches/dongfang_FC_rewrite/  
1775 4993 d 22 h /branches/dongfang_FC_rewrite/  
1645 5156 d 23 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 5172 d 0 h dongfang /branches/dongfang_FC_rewrite/ Initial import.