Subversion Repositories FlightCtrl

Rev

Rev 1612 | Show entire file | Ignore whitespace | Details | Blame | Last modification | View Log | RSS feed

Rev 1612 Rev 1614
Line 8... Line 8...
8 
0: No filter
 8 
0: No filter
9 
1: 50% new 50% old
 9 
1: 50% new 50% old
10 
2: As H&I
 10 
2: As H&I
11 
3: Reverse H&I
 11 
3: Reverse H&I
Line 12... Line 12...
12 
 
 12 
 
Line 13... Line 13...
13 
Userparam7: Yaw I factor. Default 0 (!)
 13 
Userparam7: Yaw I factor. Default 0 (may be nasty to fly!)
Line 14... Line 14...
14 
 
 14 
 
15 
Userparam8: Acc integral correction Z axis limit. Default 0 (!)
 15 
Userparam8: Acc integral correction Z axis limit. Default 0 (!)
- 
 
 16 
 
- 
 
 17 
 
16 
 
 18 
Other params:
- 
 
 19 
GyroAccFactor = 0'th order integral drift correction - acceleration sensor part as 1/1000s.
17 
 
 20 
	Default 5 (ENC-03)
Line 18... Line -...
18 
Other params:
 - 
 
19 
GyroAccFactor = Promille acc. i 0'te orden integralkorrektion. Default 5 (ENC-03)
 - 
 
20 
GyroAccTrim = Offset korrektioner divideres med dette foer det laegges til offsets. Default 2.
 21 
GyroAccTrim = -1'th order integral drift correction -
- 
 
 22 
    Offset corrections are divided by this before added to offsets. Default 2.
- 
 
 23 
DriftComp = Max offset correction per iteration (=per 1/2 second).
- 
 
 24 
    This limits the value _before_ division by GyroAccTrim! Default 32 (ENC-03)
- 
 
 25 
 
21 
DriftComp = Max offsetkorrektur pr. omgang (1/2 sek). Det er _foer_ division med GyroAccTrim! Default 32 (ENC-03)
 26 
Rotary rate limiter flag ON = dongfang axis coupling used. Otherwise H&I axis coupling