After some experimentation, the following values yield the best result. (I tested with a 30% tank level each time.)
Swaying and pitching (during rolling and braking) have been completely eliminated, and the contact points fit perfectly.
roll_MOI: Increased from just under 188,000 to 1,150,000.
Pitch_MOI: Increased from 363,000 to 1,650,000.
Suspension Damping (point.0 bis .2): The ratio (Max/Static Ratio) has been reduced from 2.5 to 2.3 (preventing the suspension from bottoming out as easily), and the damping ratio has been increased to 0.75 and 0.80, respectively, so that the nose settles smoothly after braking rather than collapsing abruptly.
[contact_points]
point.0=1, -23.63, 0.00, -7.3, 1600, 0, 0.5625, 69.8, 0.35, 2.3, 0.75, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -63.43, -6.76, -7.9, 1600, 1, 1.0, 0.0, 0.55, 2.3, 0.80, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -63.43, 6.76, -7.9, 1600, 2, 1.0, 0.0, 0.55, 2.3, 0.80, 9.0
static_pitch = -1.8
static_cg_height = 7.3
gear_system_type=1 //Hydraulic
emergency_extension_type=2 //None=0,Pump=1,Gravity=2
[WEIGHT_AND_BALANCE]
max_gross_weight = 99500 // (pounds)
empty_weight = 52230 // (pounds)
reference_datum_position = 55.35, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -56.0, 0, 7 // (feet) longitudinal, lateral,
max_number_of_stations = 50
station_load.0 = 170, -8.67, -1.4, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -8.67, 1.4, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 2500, -62.0, 0.0, 0.0 // Weight(lbs), longitudinal, late
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Passengers"
;Moments of Inertia
empty_weight_pitch_MOI = 1650000
empty_weight_roll_MOI = 1150000
empty_weight_yaw_MOI = 1850000
empty_weight_coupled_MOI = 0.0
The moments of inertia (MOI) values entered are appropriate for a light Learjet, but far too low for a heavy Global Express.
It is as if the aircraft, while on the ground, has the physical weight of a truck but the inertia of a feather—which causes it to sway excessively when cornering.