Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4341 d 12 h /branches/dongfang_FC_rewrite/  
2160 4526 d 22 h /branches/dongfang_FC_rewrite/  
2052 4637 d 9 h /branches/dongfang_FC_rewrite/  
2051 4638 d 23 h /branches/dongfang_FC_rewrite/  
2049 4639 d 22 h /branches/dongfang_FC_rewrite/  
2048 4640 d 22 h /branches/dongfang_FC_rewrite/  
2041 4645 d 21 h /branches/dongfang_FC_rewrite/  
2035 4652 d 22 h /branches/dongfang_FC_rewrite/  
1980 4792 d 1 h /branches/dongfang_FC_rewrite/  
1874 4979 d 0 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 8 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4982 d 15 h /branches/dongfang_FC_rewrite/  
1805 5086 d 8 h /branches/dongfang_FC_rewrite/  
1775 5129 d 23 h /branches/dongfang_FC_rewrite/  
1645 5293 d 1 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 1 h dongfang /branches/dongfang_FC_rewrite/ Initial import.