Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4338 d 14 h /branches/dongfang_FC_rewrite/  
2160 4524 d 0 h /branches/dongfang_FC_rewrite/  
2052 4634 d 11 h /branches/dongfang_FC_rewrite/  
2051 4636 d 1 h /branches/dongfang_FC_rewrite/  
2049 4637 d 0 h /branches/dongfang_FC_rewrite/  
2048 4638 d 0 h /branches/dongfang_FC_rewrite/  
2041 4642 d 23 h /branches/dongfang_FC_rewrite/  
2035 4650 d 0 h /branches/dongfang_FC_rewrite/  
1980 4789 d 2 h /branches/dongfang_FC_rewrite/  
1874 4976 d 2 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 4977 d 10 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 4979 d 16 h /branches/dongfang_FC_rewrite/  
1805 5083 d 10 h /branches/dongfang_FC_rewrite/  
1775 5127 d 1 h /branches/dongfang_FC_rewrite/  
1645 5290 d 3 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 5305 d 3 h dongfang /branches/dongfang_FC_rewrite/ Initial import.