Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4151 d 20 h /branches/dongfang_FC_rewrite/  
2160 4337 d 7 h /branches/dongfang_FC_rewrite/  
2052 4447 d 17 h /branches/dongfang_FC_rewrite/  
2051 4449 d 7 h /branches/dongfang_FC_rewrite/  
2049 4450 d 7 h /branches/dongfang_FC_rewrite/  
2048 4451 d 6 h /branches/dongfang_FC_rewrite/  
2041 4456 d 6 h /branches/dongfang_FC_rewrite/  
2035 4463 d 6 h /branches/dongfang_FC_rewrite/  
1980 4602 d 9 h /branches/dongfang_FC_rewrite/  
1874 4789 d 9 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 4790 d 17 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4792 d 23 h /branches/dongfang_FC_rewrite/  
1805 4896 d 17 h /branches/dongfang_FC_rewrite/  
1775 4940 d 8 h /branches/dongfang_FC_rewrite/  
1645 5103 d 9 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 5118 d 9 h dongfang /branches/dongfang_FC_rewrite/ Initial import.