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FlightCtrl
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branches
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dongfang_FC_rewrite
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invenSense.c
@ 2062
- Rev 2112
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2112
4657 d 15 h
/branches/dongfang_FC_rewrite/
2092
4665 d 2 h
/branches/dongfang_FC_rewrite/
2026
4746 d 9 h
/branches/dongfang_FC_rewrite/
2018
4763 d 12 h
/branches/dongfang_FC_rewrite/
2017
4764 d 21 h
/branches/dongfang_FC_rewrite/
2015
4765 d 5 h
/branches/dongfang_FC_rewrite/
1971
4863 d 1 h
/branches/dongfang_FC_rewrite/
1967
4863 d 18 h
/branches/dongfang_FC_rewrite/
1960
4866 d 2 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
5016 d 3 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
5048 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...)
1821
5125 d 12 h
/branches/dongfang_FC_rewrite/
reformatted.
1646
5360 d 10 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
5362 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
5377 d 3 h
dongfang
/branches/dongfang_FC_rewrite/
Initial import.