Exemplo n.º 1
0
        RendezvousTrajectory new_trajectory(double StartUT, double transfer_time)
        {
            var solver = new LambertSolver(VesselOrbit, TargetOrbit.getRelativePositionAtUT(StartUT + transfer_time), StartUT);
            var dV     = solver.dV4Transfer(transfer_time);

            return(new RendezvousTrajectory(VSL, dV, StartUT, CFG.Target, MinPeR, transfer_time));
        }
Exemplo n.º 2
0
        public static Vector3d dV4ApV(Orbit old, Vector3d ApV, double UT)
        {
            solver_s.Init(old, ApV, UT);
            var   ApR  = ApV.magnitude;
            var   minT = solver_s.ParabolicTime;
            var   maxT = solver_s.MinEnergyTime;
            var   dV   = solver_s.dV4TransferME();
            Orbit orb  = null;

            while (maxT - minT > 0.1)
            {
                var T = (maxT + minT) / 2;
                dV  = solver_s.dV4Transfer(T);
                orb = NewOrbit(old, dV, UT, orb);
                if (orb.timeToAp > T)
                {
                    minT = T;
                }
                else
                {
                    maxT = T;
                }
            }
            return(dV);
        }
        void start_orbit()
        {
            ToOrbit = null;
            var dV      = Vector3d.zero;
            var old     = VesselOrbit;
            var StartUT = VSL.Physics.UT + CorrectionOffset;

            CFG.BR.OffIfOn(BearingMode.Auto);
            update_trajectory();
            if (VesselOrbit.PeR < MinPeR)
            {
                StartUT = Math.Min(trajectory.AtTargetUT, VSL.Physics.UT + (VesselOrbit.ApAhead()? VesselOrbit.timeToAp : CorrectionOffset));
                if (trajectory.DistanceToTarget < REN.ApproachThreshold * 2 && StartUT.Equals(trajectory.AtTargetUT))
                {                 //approach is close enough to directly match orbits
                    match_orbits();
                    return;
                }
                var transfer_time = Utils.ClampL(TargetOrbit.period * (0.25 - AngleDelta(VesselOrbit, TargetOrbit, StartUT) / 360), 1);
                var solver        = new LambertSolver(VesselOrbit, TargetOrbit.getRelativePositionAtUT(StartUT + transfer_time), StartUT);
                dV = solver.dV4Transfer(transfer_time);
                var trj = new RendezvousTrajectory(VSL, dV, StartUT, CFG.Target, MinPeR, transfer_time);
                if (!dV.IsZero() && !trj.KillerOrbit)
                {                 //approach orbit is possible
                    compute_start_orbit(StartUT);
                    return;
                }
                //starting from circular orbit and proceeding to TTR fitting...
                StartUT = VesselOrbit.ApAhead()? VSL.Physics.UT + VesselOrbit.timeToAp : VSL.Physics.UT + CorrectionOffset;
                dV      = dV4C(old, hV(StartUT), StartUT);
                old     = NewOrbit(old, dV, StartUT);
            }
            else if (trajectory.RelDistanceToTarget < REN.CorrectionStart || TargetLoaded)
            {
                if (trajectory.RelDistanceToTarget > REN.CorrectionStart / 4 && !TargetLoaded)
                {
                    fine_tune_approach();
                }
                else
                {
                    match_orbits();
                }
                return;
            }
            //compute orbit with desired TTR and activate maneuver autopilot
            dV += dV4TTR(old, TargetOrbit, REN.MaxTTR, REN.MaxDeltaV, MinPeR, StartUT);
            if (!dV.IsZero())
            {
                add_node(dV, StartUT);
                CFG.AP1.On(Autopilot1.Maneuver);
            }
            stage = Stage.StartOrbit;
        }
        RendezvousTrajectory new_trajectory(double StartUT, double transfer_time)
        {
            var endUT  = StartUT + transfer_time;
            var solver = new LambertSolver(NextOrbit(endUT), NextOrbit(TargetOrbit, endUT).getRelativePositionAtUT(endUT), StartUT);

            if (solver.NotElliptic(transfer_time))
            {
                transfer_time = solver.ParabolicTime + 1;
            }
            var dV = solver.dV4Transfer(transfer_time);

            return(new RendezvousTrajectory(VSL, dV, StartUT, CFG.Target, MinPeR, transfer_time));
        }