// Update is called once per frame
void Update()
{
if (!frame1Hack)
{
frame1Hack = true;
AddGhostBodies();
ComputeBaseTransferTime();
// need GE to process these updates
Debug.LogFormat("Moon period={0:0.0}", ghostMoonOrbit[MOON_SOI_ENTER].GetPeriod());
}
if (!running)
{
// Getting user input for FR
AdjustTimeOfFlight();
UpdateManeuverSymbols();
HandleMouseSOIInput();
ComputeTransfer();
if (freeReturnInfo != null)
{
freeReturnInfo.text = string.Format("Perilune = {0:0.0}\nReturn Perigee={1:0.0}\nTime to SOI = {2:0.0}\n{3}",
ghostShipOrbit[SOI_HYPER].GetPerigee(),
ghostShipOrbit[EXIT_SOI].GetPerigee(),
timeHohmann * tflightFactor,
GravityScaler.GetWorldTimeFormatted(timeHohmann * tflightFactor, ge.units));
}
}
else
{
// RUNNING
if (Input.GetKeyUp(KeyCode.C))
{
// Circularize (if in the vicinity of the moon)
CircularizeAroundMoon();
}
else if (Input.GetKeyUp(KeyCode.R))
{
// Raise circular orbit but Hohmann Xfer
NewCircularOrbit(1.3f);
}
return;
}
if (Input.GetKeyUp(KeyCode.X))
{
// execute the transfer
ExecuteTransfer();
if (instructions != null)
{
instructions.gameObject.SetActive(false);
}
running = true;
}
else if (Input.GetKeyUp(KeyCode.Space))
{
ge.SetEvolve(!ge.GetEvolve());
}
}
void FixedUpdate()
{
if (!running)
{
running = true;
gravityEngine.SetEvolve(true);
}
}
private void ExecuteTransfer()
{
// Need to account for phasing, rotate ship forward to correct launch point and
// rotate TLI vector. (This assumes circular orbit in the XY plane with the planet at the origin!)
// Should set as a maneuver, but just jump there for demonstration code
double transferTime = tflightFactor * lambertU.GetTMin();
float moonOmega = (float)System.Math.Sqrt(ge.GetMass(planet)) / Mathf.Sqrt(moonRadius * moonRadius * moonRadius);
float shipThetaDeg = (float)(transferTime * moonOmega) * Mathf.Rad2Deg;
Debug.LogFormat("t={0} theta={1} deg. omega={2} rad", transferTime, shipThetaDeg, moonOmega);
// Inclination support. Recompute the transfer using inclination
// @TODO: HACK XY only
Vector3 shipPos = ge.GetPhysicsPosition(spaceship);
Vector3 shipPosPhased = Quaternion.AngleAxis(shipThetaDeg, Vector3.forward) * shipPos;
Vector3 shipVelPhased = Quaternion.AngleAxis(shipThetaDeg, Vector3.forward) * lambertU.GetTransferVelocity();
if (onRails)
{
TransferOnRails(transferTime, shipPosPhased, shipVelPhased, moonOmega);
}
else
{
Debug.LogFormat("tli NBody mode r={0} v={1}", shipPosPhased, shipVelPhased);
ge.UpdatePositionAndVelocity(spaceship, shipPosPhased, shipVelPhased);
}
// remove placeholder ships/orbit visualizers
ge.RemoveBody(shipExitSOI.gameObject);
shipExitSOI.gameObject.SetActive(false);
ge.RemoveBody(shipEnterSOI.gameObject);
shipEnterSOI.gameObject.SetActive(false);
SetOrbitDisplays(false);
ge.SetEvolve(true);
running = true;
}
