Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4361 d 2 h /branches/dongfang_FC_rewrite/  
2160 4546 d 12 h /branches/dongfang_FC_rewrite/  
2052 4656 d 23 h /branches/dongfang_FC_rewrite/  
2051 4658 d 13 h /branches/dongfang_FC_rewrite/  
2049 4659 d 12 h /branches/dongfang_FC_rewrite/  
2048 4660 d 11 h /branches/dongfang_FC_rewrite/  
2041 4665 d 11 h /branches/dongfang_FC_rewrite/  
2035 4672 d 11 h /branches/dongfang_FC_rewrite/  
1980 4811 d 14 h /branches/dongfang_FC_rewrite/  
1874 4998 d 14 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 4999 d 22 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 5002 d 4 h /branches/dongfang_FC_rewrite/  
1805 5105 d 22 h /branches/dongfang_FC_rewrite/  
1775 5149 d 13 h /branches/dongfang_FC_rewrite/  
1645 5312 d 15 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 5327 d 15 h dongfang /branches/dongfang_FC_rewrite/ Initial import.