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FlightCtrl
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dongfang_FC_rewrite
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invenSense.c
@ 1652
- Rev 2112
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2112
4583 d 11 h
/branches/dongfang_FC_rewrite/
2092
4590 d 21 h
/branches/dongfang_FC_rewrite/
2026
4672 d 5 h
/branches/dongfang_FC_rewrite/
2018
4689 d 7 h
/branches/dongfang_FC_rewrite/
2017
4690 d 17 h
/branches/dongfang_FC_rewrite/
2015
4691 d 1 h
/branches/dongfang_FC_rewrite/
1971
4788 d 20 h
/branches/dongfang_FC_rewrite/
1967
4789 d 13 h
/branches/dongfang_FC_rewrite/
1960
4791 d 22 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
4941 d 22 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
4973 d 22 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
5051 d 8 h
/branches/dongfang_FC_rewrite/
reformatted.
1646
5286 d 5 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
5287 d 22 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
5302 d 22 h
dongfang
/branches/dongfang_FC_rewrite/
Initial import.