Subversion Repositories FlightCtrl

Rev

Go to most recent revision | Show changed files | Details | Compare with Previous | Blame | RSS feed

Filtering Options

Rev Age Author Path Log message Diff
2052 4503 d 21 h /branches/dongfang_FC_rewrite/  
2051 4505 d 11 h /branches/dongfang_FC_rewrite/  
2049 4506 d 11 h /branches/dongfang_FC_rewrite/  
2048 4507 d 10 h /branches/dongfang_FC_rewrite/  
2041 4512 d 10 h /branches/dongfang_FC_rewrite/  
2035 4519 d 10 h /branches/dongfang_FC_rewrite/  
1980 4658 d 13 h /branches/dongfang_FC_rewrite/  
1874 4845 d 13 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 4846 d 21 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4849 d 3 h /branches/dongfang_FC_rewrite/  
1805 4952 d 21 h /branches/dongfang_FC_rewrite/  
1775 4996 d 12 h /branches/dongfang_FC_rewrite/  
1645 5159 d 13 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 5174 d 14 h dongfang /branches/dongfang_FC_rewrite/ Initial import.