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Titan2Tests.cs
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Titan2Tests.cs
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/*
* Copyright Lamont Granquist (lamont@scriptkiddie.org)
* Dual licensed under the MIT (MIT-LICENSE) license
* and GPLv2 (GPLv2-LICENSE) license or any later version.
*/
using System;
using AssertExtensions;
using MechJebLib.Primitives;
using MechJebLib.PVG;
using Xunit;
using static MechJebLib.Utils.Statics;
namespace MechJebLibTest.PVG
{
public class Titan2Tests
{
// this is a forced periapsis attachment problem, which chooses an ApR such that it winds up burning the whole rocket.
[Fact]
public void FlightPathAngle4AllRocket()
{
var r0 = new V3(5593203.65707947, 0, 3050526.81522927);
var v0 = new V3(0, 407.862893197274, 0);
double t0 = 0;
double PeR = 6.371e+6 + 185e+3;
double ApR = 6.371e+6 + 4306022;
double rbody = 6.371e+6;
double incT = Deg2Rad(28.608);
double mu = 3.986004418e+14;
Ascent ascent = Ascent.Builder()
.AddStageUsingThrust(153180, 2194400, 296, 156, 4, 4)
.AddStageUsingThrust(31980, 443700, 315, 180, 3, 3, true)
.Initial(r0, v0, r0.normalized, t0, mu, rbody)
.SetTarget(PeR, ApR, PeR, incT, Deg2Rad(270), 0, true, false)
.Build();
ascent.Run();
Optimizer pvg = ascent.GetOptimizer() ?? throw new Exception("null optimzer");
using Solution solution = pvg.GetSolution();
(V3 rf, V3 vf) = solution.TerminalStateVectors();
(double smaf, double eccf, double incf, double lanf, double argpf, double tanof, _) =
MechJebLib.Core.Maths.KeplerianFromStateVectors(mu, rf, vf);
solution.R(0).ShouldEqual(r0);
solution.V(0).ShouldEqual(v0);
solution.M(0).ShouldEqual(153180);
solution.Constant(0).ShouldBeZero(1e-7);
solution.Constant(solution.tmax).ShouldBeZero(1e-7);
solution.Vgo(0).ShouldEqual(9327.0948576056289, 1e-7);
solution.Pv(0).ShouldEqual(new V3(0.24913591286181805, 0.23909088173239779, 0.13587844086293846), 1e-7);
pvg.Znorm.ShouldBeZero(1e-9);
smaf.ShouldEqual(8616511.1913318466, 1e-7);
eccf.ShouldEqual(0.23913520746130185, 1e-7);
incf.ShouldEqual(incT, 1e-7);
lanf.ShouldEqual(Deg2Rad(270), 1e-7);
argpf.ShouldEqual(1.7637313812499942, 1e-7);
ClampPi(tanof).ShouldBeZero(1e-7);
}
// this is FlightPathAngle4AllRocket but using free attachment.
[Fact]
public void Kepler3()
{
var r0 = new V3(5593203.65707947, 0, 3050526.81522927);
var v0 = new V3(0, 407.862893197274, 0);
double t0 = 0;
double PeR = 6.371e+6 + 185e+3;
double ApR = 6.371e+6 + 4306022;
;
double rbody = 6.371e+6;
double incT = Deg2Rad(28.608);
double mu = 3.986004418e+14;
Ascent ascent = Ascent.Builder()
.AddStageUsingThrust(157355.487476332, 2340000, 301.817977905273, 148.102380138703, 4, 4)
.AddStageUsingThrust(32758.6353093992, 456100.006103516, 315.000112652779, 178.63040653022, 3, 3, true)
.Initial(r0, v0, r0.normalized, t0, mu, rbody)
.SetTarget(PeR, ApR, PeR, incT, Deg2Rad(270), 0, false, false)
.Build();
ascent.Run();
Optimizer pvg = ascent.GetOptimizer() ?? throw new Exception("null optimzer");
Solution solution = pvg.GetSolution();
(V3 rf, V3 vf) = solution.TerminalStateVectors();
(double smaf, double eccf, double incf, double lanf, double argpf, double tanof, _) =
MechJebLib.Core.Maths.KeplerianFromStateVectors(mu, rf, vf);
solution.R(0).ShouldEqual(r0);
solution.V(0).ShouldEqual(v0);
solution.M(0).ShouldEqual(157355.487476332);
solution.Constant(0).ShouldBeZero(1e-7);
solution.Constant(solution.tmax).ShouldBeZero(1e-7);
solution.Vgo(0).ShouldEqual(9291.2315891261242, 1e-7);
solution.Pv(0).ShouldEqual(new V3(0.25236763236272763, 0.24870860524790397, 0.13764101483910374), 1e-7);
pvg.Znorm.ShouldBeZero(1e-9);
smaf.ShouldEqual(8616511.1913318466, 1e-7);
eccf.ShouldEqual(0.23913520746130185, 1e-7);
incf.ShouldEqual(incT, 1e-7);
lanf.ShouldEqual(Deg2Rad(270), 1e-7);
argpf.ShouldEqual(1.6667949762852059, 1e-7);
ClampPi(tanof).ShouldEqual(0.090826664012324976, 1e-7);
}
// target a 185x186 without getting apopasis attachment. unfortuantely, i don't have a use case that
// exercizes the logic to re-pin to the periapsis because it grabs the apopasis incorrectly.
[Fact]
public void Kepler3NoApoapsisAttachment()
{
var r0 = new V3(5593203.65707947, 0, 3050526.81522927);
var v0 = new V3(0, 407.862893197274, 0);
double t0 = 0;
double PeR = 6.371e+6 + 185e+3;
double ApR = 6.371e+6 + 186e+3;
double rbody = 6.371e+6;
double incT = Deg2Rad(28.608);
double mu = 3.986004418e+14;
Ascent ascent = Ascent.Builder()
.AddStageUsingThrust(157355.487476332, 2340000, 301.817977905273, 148.102380138703, 4, 4)
.AddStageUsingThrust(32758.6353093992, 456100.006103516, 315.000112652779, 178.63040653022, 3, 3, true)
.Initial(r0, v0, r0.normalized, t0, mu, rbody)
.SetTarget(PeR, ApR, PeR, incT, Deg2Rad(270), 0, false, false)
.Build();
ascent.Run();
Optimizer pvg = ascent.GetOptimizer() ?? throw new Exception("null optimzer");
Solution solution = pvg.GetSolution();
(V3 rf, V3 vf) = solution.TerminalStateVectors();
(double smaf, double eccf, double incf, double lanf, double argpf, double tanof, _) =
MechJebLib.Core.Maths.KeplerianFromStateVectors(mu, rf, vf);
solution.R(0).ShouldEqual(r0);
solution.V(0).ShouldEqual(v0);
solution.M(0).ShouldEqual(157355.487476332);
solution.Constant(0).ShouldBeZero(1e-7);
solution.Constant(solution.tmax).ShouldBeZero(1e-7);
solution.Vgo(0).ShouldEqual(8498.9352440057573, 1e-7);
solution.Pv(0).ShouldEqual(new V3(0.24009395607850137, 0.21526467329187604, 0.13094696426599889), 1e-7);
double aprf = MechJebLib.Core.Maths.ApoapsisFromKeplerian(smaf, eccf);
double perf = MechJebLib.Core.Maths.PeriapsisFromKeplerian(smaf, eccf);
perf.ShouldEqual(PeR, 1e-9);
aprf.ShouldEqual(ApR, 1e-9);
pvg.Znorm.ShouldBeZero(1e-9);
smaf.ShouldEqual(6556500.0000104867, 1e-7);
eccf.ShouldEqual(7.6259809968559891E-05, 1e-7);
incf.ShouldEqual(incT, 1e-7);
lanf.ShouldEqual(Deg2Rad(270), 1e-7);
argpf.ShouldEqual(1.6494150858682159, 1e-7);
tanof.ShouldEqual(0.09094016908398217, 1e-7);
}
}
}