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FlightCtrl
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dongfang_FC_rewrite
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invenSense.c
@ 1619
- Rev 2112
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2112
4661 d 4 h
/branches/dongfang_FC_rewrite/
2092
4668 d 15 h
/branches/dongfang_FC_rewrite/
2026
4749 d 22 h
/branches/dongfang_FC_rewrite/
2018
4767 d 0 h
/branches/dongfang_FC_rewrite/
2017
4768 d 10 h
/branches/dongfang_FC_rewrite/
2015
4768 d 18 h
/branches/dongfang_FC_rewrite/
1971
4866 d 13 h
/branches/dongfang_FC_rewrite/
1967
4867 d 6 h
/branches/dongfang_FC_rewrite/
1960
4869 d 15 h
/branches/dongfang_FC_rewrite/
Parameter set changed - no longer MK compatible.
EEPROM data format changed - no longer MK compatible. Has checksum, and only one shared R/C channel map.
1887
5019 d 16 h
/branches/dongfang_FC_rewrite/
Performance problem solved (int32 mul and div removed where possible)
Beeper output moved from configuration module to output module for future combination with LED output signals
setDelay, delay methods properly camel cased
1874
5051 d 15 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...)
1821
5129 d 1 h
/branches/dongfang_FC_rewrite/
reformatted.
1646
5363 d 22 h
/branches/dongfang_FC_rewrite/
Gyro and acc. offsetting rewritten. Now it is jolt-free. Offsets are unsigned.
New defaults for drift compensation.
Bug in acc. and gyro fusion fixed.
All gyro types tested (a standard FC1.3, a standard FC2.0 and a nonstandard InvenSense FC)
1645
5365 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
5380 d 16 h
dongfang
/branches/dongfang_FC_rewrite/
Initial import.