public override void Update(float deltaTime)
{
Vector2 acc = CalculateAcceleration(MCentreBaseOfGravity.Position, MSatelliteBaseEntity.Position);
Vector2 deltaAcc = acc * deltaTime;
Vector2 adjustment = (m_orbit[m_currentOrbitIndex] - MSatelliteBaseEntity.Position) * m_adjustmentStrength;
Vector2 adjustedAcc = adjustment.magnitude > 0.1f ? adjustment
: adjustment + MSatelliteBaseEntity.Velocity + deltaAcc;
MSatelliteBaseEntity.SetVelocity(adjustedAcc);
m_currentOrbitIndex = ++m_currentOrbitIndex % m_orbit.Count;
}
public override void Update(float deltaTime)
{
base.Update(deltaTime);
float currentRotationAngleZ = MSatelliteBaseEntity.Rotation.eulerAngles.z;
if (Input.GetKey(KeyCode.A))
{
MSatelliteBaseEntity.SetRotation(
Quaternion.AngleAxis(currentRotationAngleZ + m_turnAngle, Vector3.forward));
}
else if (Input.GetKey(KeyCode.D))
{
MSatelliteBaseEntity.SetRotation(
Quaternion.AngleAxis(currentRotationAngleZ - m_turnAngle, Vector3.forward));
}
if (Input.GetKey(KeyCode.Space))
{
MSatelliteBaseEntity.SetVelocity(MSatelliteBaseEntity.Velocity + (Vector2)(MSatelliteBaseEntity.Rotation * m_acceleration));
}
}
