For a Helicopter landing on an undercarriage system modeled as a single spring damper.
In principle, is it possible to determine K and C values for a single (constant rate) spring damper system given the mass of the helicopter and 2 independent scenarios of initial velocity (touch down) values each with an associated maximum allowable deceleration value. No spring length is specified. No forcing term is present.
Just trying not to waste (anymore) time heading in the wrong direction.
I'm not looking for specific solutions.