示例#1
0
        internal override void ActionCommand(Game game)
        {
            if (!IsRunning)
            {
                Entity  parentEntity = EntityCommanding.GetDataBlob <OrbitDB>().Parent;
                Vector2 newVector    = OrbitProcessor.InstantaneousOrbitalVelocityVector(EntityCommanding.GetDataBlob <OrbitDB>(), _db.ActionOnDateTime);
                newVector += _db.DeltaVToExpend_AU;
                var     spdmps      = Distance.AuToMt(newVector.Length());
                Vector3 newVector3d = new Vector3(newVector.X, newVector.Y, 0);
                OrbitDB newOrbit    = OrbitDB.FromVector(parentEntity, EntityCommanding, newVector3d, _db.ActionOnDateTime);

                /*
                 * if (newOrbit.Periapsis > targetSOI)
                 * {
                 *  //TODO: find who's SOI we're currently in and create an orbit for that;
                 * }
                 * if (newOrbit.Apoapsis > targetSOI)
                 * {
                 *  //TODO: change orbit to new parent at SOI change
                 * }
                 */


                EntityCommanding.SetDataBlob(newOrbit);
                newOrbit.SetParent(parentEntity);
            }
        }
示例#2
0
        /// <summary>
        /// This was designed so that fast moving objects will get interpolated a lot more than slow moving objects
        /// so fast moving objects shouldn't loose positional acuracy when close to a planet,
        /// and slow moving objects won't have processor time wasted on them by calulcating too often.
        /// However this seems to be unstable and looses energy, unsure why. currently set it to just itterate/interpolate every second.
        /// so currently will be using more time to get through this than neccisary.
        /// </summary>
        /// <param name="entity">Entity.</param>
        /// <param name="deltaSeconds">Delta seconds.</param>
        public static void NewtonMove(Entity entity, int deltaSeconds)
        {
            NewtonMoveDB newtonMoveDB  = entity.GetDataBlob <NewtonMoveDB>();
            PositionDB   positionDB    = entity.GetDataBlob <PositionDB>();
            double       Mass_Kg       = entity.GetDataBlob <MassVolumeDB>().Mass;
            double       ParentMass_kg = newtonMoveDB.ParentMass;

            var      manager        = entity.Manager;
            DateTime dateTimeFrom   = newtonMoveDB.LastProcessDateTime;
            DateTime dateTimeNow    = manager.ManagerSubpulses.StarSysDateTime;
            DateTime dateTimeFuture = dateTimeNow + TimeSpan.FromSeconds(deltaSeconds);
            double   deltaT         = (dateTimeFuture - dateTimeFrom).TotalSeconds;

            double secondsToItterate = deltaT;

            while (secondsToItterate > 0)
            {
                double speed_kms = newtonMoveDB.CurrentVector_kms.Length();


                //double timeStep = Math.Max(secondsToItterate / speed_kms, 1);
                //timeStep = Math.Min(timeStep, secondsToItterate);
                double timeStep           = 1;//because the above seems unstable and looses energy.
                double distanceToParent_m = Distance.AuToMt(positionDB.GetDistanceTo(newtonMoveDB.SOIParent.GetDataBlob <PositionDB>()));

                distanceToParent_m = Math.Max(distanceToParent_m, 0.1); //don't let the distance be 0 (once collision is in this will likely never happen anyway)

                double  gravForce       = GameConstants.Science.GravitationalConstant * (Mass_Kg * ParentMass_kg / Math.Pow(distanceToParent_m, 2));
                Vector3 gravForceVector = gravForce * -Vector3.Normalise(positionDB.RelativePosition_AU);
                double  distance        = Distance.AuToKm(positionDB.RelativePosition_AU).Length();
                Vector3 totalForce      = gravForceVector + newtonMoveDB.ThrustVector;

                Vector3 acceleration_mps = totalForce / Mass_Kg;
                Vector3 newVelocity      = (acceleration_mps * timeStep * 0.001) + newtonMoveDB.CurrentVector_kms;

                newtonMoveDB.CurrentVector_kms = newVelocity;
                Vector3 deltaPos = (newtonMoveDB.CurrentVector_kms + newVelocity) / 2 * timeStep;
                //Vector4 deltaPos = newtonMoveDB.CurrentVector_kms * timeStep;

                positionDB.RelativePosition_AU += Distance.KmToAU(deltaPos);

                double sOIRadius_AU = OrbitProcessor.GetSOI(newtonMoveDB.SOIParent);

                if (positionDB.RelativePosition_AU.Length() >= sOIRadius_AU)
                {
                    Entity  newParent;
                    Vector3 parentRalitiveVector;
                    //if our parent is a regular kepler object (normaly this is the case)
                    if (newtonMoveDB.SOIParent.HasDataBlob <OrbitDB>())
                    {
                        var orbitDB = newtonMoveDB.SOIParent.GetDataBlob <OrbitDB>();
                        newParent = orbitDB.Parent;
                        var parentVelocity = OrbitProcessor.InstantaneousOrbitalVelocityVector(orbitDB, entity.Manager.ManagerSubpulses.StarSysDateTime);
                        parentRalitiveVector = Distance.KmToAU(newtonMoveDB.CurrentVector_kms) + parentVelocity;
                        var pvlen = Distance.AuToKm(parentVelocity.Length());
                        var vlen  = newtonMoveDB.CurrentVector_kms.Length();
                        var rvlen = Distance.AuToKm(parentRalitiveVector.Length());
                    }
                    else //if (newtonMoveDB.SOIParent.HasDataBlob<NewtonMoveDB>())
                    {   //this will pretty much never happen.
                        newParent = newtonMoveDB.SOIParent.GetDataBlob <NewtonMoveDB>().SOIParent;
                        var parentVelocity = newtonMoveDB.SOIParent.GetDataBlob <NewtonMoveDB>().CurrentVector_kms;
                        parentRalitiveVector = Distance.KmToAU(newtonMoveDB.CurrentVector_kms + parentVelocity);
                    }
                    double  newParentMass          = newParent.GetDataBlob <MassVolumeDB>().Mass;
                    double  sgp                    = GameConstants.Science.GravitationalConstant * (newParentMass + Mass_Kg) / 3.347928976e33;
                    Vector3 posRalitiveToNewParent = positionDB.AbsolutePosition_AU - newParent.GetDataBlob <PositionDB>().AbsolutePosition_AU;

                    var dateTime = dateTimeNow + TimeSpan.FromSeconds(deltaSeconds - secondsToItterate);
                    var kE       = OrbitMath.KeplerFromPositionAndVelocity(sgp, posRalitiveToNewParent, parentRalitiveVector, dateTime);

                    if (kE.Eccentricity < 1) //if we're going to end up in a regular orbit around our new parent
                    {
                        /*
                         * var newOrbit = OrbitDB.FromKeplerElements(
                         *  newParent,
                         *  newParentMass,
                         *  Mass_Kg,
                         *  kE,
                         *  dateTime);
                         */
                        var newOrbit = OrbitDB.FromVector(newParent, entity, parentRalitiveVector, dateTime);
                        entity.RemoveDataBlob <NewtonMoveDB>();
                        entity.SetDataBlob(newOrbit);
                        positionDB.SetParent(newParent);
                        var currentPos = Distance.AuToKm(positionDB.RelativePosition_AU);
                        var newPos     = OrbitProcessor.GetPosition_AU(newOrbit, dateTime);
                        var newPosKM   = Distance.AuToKm(newPos);
                        positionDB.RelativePosition_AU = newPos;
                        break;
                    }
                    else //else we're in a hyperbolic trajectory around our new parent, so just coninue the newtonion move.
                    {
                        positionDB.SetParent(newParent);
                        newtonMoveDB.ParentMass = newParentMass;
                        newtonMoveDB.SOIParent  = newParent;
                    }
                }
                secondsToItterate -= timeStep;
            }
            newtonMoveDB.LastProcessDateTime = dateTimeFuture;
        }