diff --git a/Systems/jsb-controls.xml b/Systems/jsb-controls.xml index a0df4837..9bf88495 100644 --- a/Systems/jsb-controls.xml +++ b/Systems/jsb-controls.xml @@ -6,9 +6,14 @@ begin: control system by Nikolai V. Chr. AD-A055-417 - Main source. + Pitch error gain = 3.0 AD-A189-675 - Some parts of this used (except for in the YF-16). + Pitch error gain = 0.7 + Made by LJQC TP-1538 - used for control system B/C and non-prototype gains. - TN-D-8176 - used for servodynamic filters. Disabled for now (fdm rate is only 120Hz). + Pitch error gain = 1.5 + TN-D-8176 - used for servodynamic filters. Disabled for now as all 5 is not damped enough. + Pitch error gain = 2.5 ICAS-90-5.10.2 - used for MPO switch AFSC 32657C - has more clean view of Integrator pitch loop. --> @@ -1118,7 +1123,7 @@ - + fcs/fly-by-wire/pitch/normal-1-special 0.5 @@ -1132,13 +1137,14 @@ + + fcs/fly-by-wire/pitch/q-washout 0.167 - + - Niko: See reason for this in q-lagged component. velocities/q-deg_sec 0.25 @@ -1159,7 +1165,7 @@ LJQC: (AOA - 10)*0.105, take pos val, and adds to the pitch rate feedback path. - The gain is 0.105, cross checked with BMS developer mav-jp. + The gain is 0.105, cross checked with BMS developer mav-jp. fcs/fly-by-wire/pitch/pitch-rate-cmd-sum-1987 0.0525 @@ -1173,7 +1179,7 @@ LJQC: the washed-out pitch rate is not added to this path. - fcs/fly-by-wire/pitch/q-lagged-gained-1987 + fcs/fly-by-wire/pitch/q-gained-1987 fcs/fly-by-wire/pitch/pitch-rate-cmd-gained-1987 @@ -1184,7 +1190,7 @@ fcs/fly-by-wire/pitch/q-washout-gained-1987 - fcs/fly-by-wire/pitch/normal-gain + fcs/fly-by-wire/pitch/normal-1-gain-half @@ -1199,7 +1205,7 @@ - + fcs/fly-by-wire/ada189675 == 1 @@ -3175,7 +3181,7 @@ fcs/fly-by-wire/tef/sum - 8 + 8