Disable aircraft flightmodel changes (#5167)

* Disable aircraft flightmodel changes

* Remove files
This commit is contained in:
PabstMirror 2017-05-16 21:40:24 -05:00 committed by GitHub
parent 9ba3b5aa6a
commit f7d9a165f6
4 changed files with 0 additions and 73 deletions

View File

@ -223,25 +223,16 @@ class CfgVehicles {
class Plane_CAS_01_base_F: Plane_Base_F {
lockDetectionSystem = 12;
incomingMissileDetectionSystem = 16;
class Turrets;
#include <flightmodel_thunderbolt.hpp>
};
class Plane_CAS_02_base_F: Plane_Base_F {
lockDetectionSystem = 12;
incomingMissileDetectionSystem = 16;
class Turrets;
#include <flightmodel_yak.hpp>
};
class Plane_Fighter_03_base_F: Plane_Base_F {
lockDetectionSystem = 12;
incomingMissileDetectionSystem = 16;
class Turrets;
#include <flightmodel_alca.hpp>
};
class UAV_01_base_F: Helicopter_Base_F {

View File

@ -1,23 +0,0 @@
acceleration = 300;
maxSpeed = 936;
irScanRangeMin = 500;
irScanRangeMax = 5000;
aileronSensitivity = 0.64;
elevatorSensitivity = 0.682;
rudderInfluence = 0.001;
aileronControlsSensitivityCoef = 3;
elevatorControlsSensitivity = 2;
rudderControlsSensitivityoef = 4;
elevatorCoef[] = {0.6, 0.73, 0.62, 0.52, 0.39, 0.33, 0.28};
aileronCoef[] = {0.5, 0.68, 0.75, 0.86, 0.92, 0.96, 1};
rudderCoef[] = {0.9, 0.75, 0.58, 0.45, 0.38, 0.35, 0.3};
envelope[] = {0, 0.06, 1.2, 3, 3.6, 3.75, 3.65, 3.45, 3.3, 2.8, 2.4, 1.9, 1.5};
angleOfIndicence = 0.0523599; //determines velocity vector behaviour, how quickly it catches up with where your nose is pointing, I think
draconicForceXCoef = 7.5; //max angle of attack, lower value gives higher aoa
draconicForceYCoef = 0.2198; //Something to do with bleed off of speed, low values seem to increase bleed off
draconicForceZCoef = 5.12; //????
draconicTorqueXCoef = 0.18; //resistance to elevator input, also impacts speed degradation
draconicTorqueYCoef = 0.000017;
thrustCoef[] = {1.3, 1.27, 1.24, 1.2, 1.17, 1.15, 1.13, 1.1, 1.06, 1, 0.94, 0.72, 0.51, 0.4, 0.25, 0};
gunAimDown = 0.029;
flapsFrictionCoef = 0.32;

View File

@ -1,21 +0,0 @@
maxSpeed = 736;
aileronSensitivity = 0.85;
elevatorSensitivity = 0.75;
rudderInfluence = 0.001;
aileronControlsSensitivityCoef = 3;
elevatorControlsSensitivity = 2;
rudderControlsSensitivityoef = 4;
elevatorCoef[] = {0.7, 0.75, 0.75, 0.65, 0.55, 0.45, 0.35};
aileronCoef[] = {0.6, 0.85, 0.88, 0.92, 0.95, 0.97, 1};
rudderCoef[] = {0.8, 0.75, 0.65, 0.5, 0.4, 0.33, 0.3};
flapsFrictionCoef = 0.35;
angleOfIndicence = 0.0523599;
draconicForceXCoef = 9.5;
draconicForceYCoef = 0.56;
draconicForceZCoef = 0.1;
draconicTorqueXCoef = 0.58;
draconicTorqueYCoef = 0.00013;
envelope[] = {0, 0, 0.75, 2.4, 3.6, 3.8, 3.7, 3.2, 2.2, 1.7, 0.9};
thrustCoef[] = {1, 1.2, 1.3, 1.25, 1.06, 1.01, 1, 0.92, 0.75, 0.65, 0.5, 0.25, 0};
acceleration = 265;
landingSpeed = 220;

View File

@ -1,20 +0,0 @@
maxSpeed = 1059;
acceleration = 300;
aileronSensitivity = 0.635;
elevatorSensitivity = 0.814;
rudderInfluence = 0.001;
aileronControlsSensitivityCoef = 3;
elevatorControlsSensitivity = 2;
rudderControlsSensitivityoef = 4;
elevatorCoef[] = {0.6, 0.76, 0.7, 0.65, 0.58, 0.47, 0.43};
aileronCoef[] = {0.5, 0.85, 0.87, 0.89, 0.92, 0.95, 1};
rudderCoef[] = {0.8, 0.7, 0.6, 0.5, 0.4, 0.32, 0.27};
angleOfIndicence = 0.0523599;
draconicForceXCoef = 7.6;
draconicForceYCoef = 0.75;
draconicForceZCoef = 0.085;
draconicTorqueXCoef = 0.815;
draconicTorqueYCoef = 0.000152;
envelope[] = {0, 0.446, 1.5, 3.9, 5.2, 4.8, 4.2, 3.5, 2, 1, 0.5};
thrustCoef[] = {1, 1.2, 1.7, 1.7, 1.65, 1.54, 1.32, 1.1, 0.95, 0.75, 0.5, 0.35, 0};
flapsFrictionCoef = 0.32;