Subversion Repositories FlightCtrl

Rev

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

Filtering Options

Rev Age Author Path Log message Diff
2189 4389 d 19 h /branches/dongfang_FC_rewrite/  
2160 4575 d 6 h /branches/dongfang_FC_rewrite/  
2052 4685 d 16 h /branches/dongfang_FC_rewrite/  
2051 4687 d 6 h /branches/dongfang_FC_rewrite/  
2049 4688 d 6 h /branches/dongfang_FC_rewrite/  
2048 4689 d 5 h /branches/dongfang_FC_rewrite/  
2041 4694 d 5 h /branches/dongfang_FC_rewrite/  
2035 4701 d 5 h /branches/dongfang_FC_rewrite/  
1980 4840 d 8 h /branches/dongfang_FC_rewrite/  
1874 5027 d 8 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 5028 d 16 h /branches/dongfang_FC_rewrite/ Performance problems fixed.  
1869 5030 d 22 h /branches/dongfang_FC_rewrite/  
1805 5134 d 16 h /branches/dongfang_FC_rewrite/  
1775 5178 d 7 h /branches/dongfang_FC_rewrite/  
1645 5341 d 8 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 5356 d 9 h dongfang /branches/dongfang_FC_rewrite/ Initial import.