remove unused script
continuous-integration/drone/push Build is passing
Details
continuous-integration/drone/push Build is passing
Details
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/*
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credit Nerdu#7492 from the Dev Submarine
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its a little unreadable
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so im gonna do my best to remember and explan
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explain*
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so the calculate initial orbital params does p much what it says it does
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so u can get the initial true anomaly p easy via the initial position
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but im p sure it becomes a bit more complicated if u want to solve for it in the future
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so you have to calculate initial mean and eccentric anomaly
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and then once thats done, i just use the RecalculateAtTime to update the ships current variables, like its flight path and other stuff, and the GetPositionAtTime() function to get the position at any time to draw the orbit. This is done by simply getting mean anomaly at any time and then converting to true anomaly, and then its p simply from there
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im p sure some of the equations are a little diff from what i was finding online because i had to tweak them to my sims needs or i had to like add 90 degrees or something stupid like that
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but yea otherwise u should be able to take a lot off of this script
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its p ugly
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its practically a singleton 💀
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also i think i had to custom write the Cosh, Sinh, Tanh, Atanh, Acosh, and Asinh functions
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lemme find them
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if u want the whole project to see it in action just lemme know
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im p sure it was slightly buggy at times but not the worst
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*/
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public class spaceshipScript : MonoBehaviour
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{
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private Camera cam;
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private LineRenderer orbitLR;
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private LineRenderer shipToPlanetLR;
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private LineRenderer velocityLR;
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private LineRenderer perpRLR;
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public float mouseScrollMultiplier;
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public AnimationCurve curveForMouseZoom;
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public float maxMouseZoomMultiplier;
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public float minZoom;
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public float maxZoom;
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public Transform orbitedPlanet;
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public celestialBodyScript orbitedPlanetScript;
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private Rigidbody2D rb;
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public Vector2 initVelocity;
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public OrbitalParameters currentOrbitalParams;
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private orbitSimulationManager simManager;
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public float orbitDrawnMaxWidth;
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public AnimationCurve orbitDrawnWidthCurve;
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public float thrustVelocity;
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public float rotationSpeed;
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//km
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public float physicsDistance;
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// Start is called before the first frame update
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void Start()
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{
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orbitLR = transform.GetChild(0).GetComponent<LineRenderer>();
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shipToPlanetLR = transform.GetChild(1).GetComponent<LineRenderer>();
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velocityLR = transform.GetChild(2).GetComponent<LineRenderer>();
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perpRLR = transform.GetChild(3).GetComponent<LineRenderer>();
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simManager = GameObject.FindGameObjectWithTag("simManager").GetComponent<orbitSimulationManager>();
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cam = Camera.main;
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rb = GetComponent<Rigidbody2D>();
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rb.velocity = initVelocity / simManager.scale;
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Vector2 posFromPlanet = (Vector2)transform.position - (Vector2) orbitedPlanet.position;
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posFromPlanet *= simManager.scale;
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CalculateOrbitalParams(
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new Vector2d((double)initVelocity.x,
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(double)initVelocity.y),
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new Vector2d(posFromPlanet.x, posFromPlanet.y),
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orbitedPlanetScript.mass,
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true);
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}
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// Update is called once per frame
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void Update()
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{
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if (Input.GetKey(KeyCode.A))
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{
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transform.Rotate(0f,0f,rotationSpeed * Time.deltaTime * simManager.timeScale);
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}
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if (Input.GetKey(KeyCode.D))
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{
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transform.Rotate(0f,0f,-rotationSpeed * Time.deltaTime * simManager.timeScale);
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}
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ZoomOrthoCamera();
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float orbitWidthVal = orbitDrawnMaxWidth * orbitDrawnWidthCurve.Evaluate(cam.orthographicSize / maxZoom);
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orbitLR.startWidth = orbitWidthVal;
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orbitLR.endWidth = orbitWidthVal;
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shipToPlanetLR.startWidth = orbitWidthVal;
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shipToPlanetLR.endWidth = orbitWidthVal;
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velocityLR.startWidth = orbitWidthVal;
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velocityLR.endWidth = orbitWidthVal;
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perpRLR.startWidth = orbitWidthVal;
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perpRLR.endWidth = orbitWidthVal;
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}
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private void FixedUpdate()
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{
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Vector2d dir = new Vector2d(Mathd.Cos((double)transform.rotation.eulerAngles.z * Mathd.Deg2Rad), Mathd.Sin((double)transform.rotation.eulerAngles.z * Mathd.Deg2Rad));
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if (Input.GetKey(KeyCode.Space))
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{
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if (Vector2.Distance(transform.position, orbitedPlanet.position) > (orbitedPlanetScript.radius + physicsDistance)/simManager.scale)
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{
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Vector2 posFromPlanet = (Vector2)transform.position - (Vector2) orbitedPlanet.position;
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if (simManager.timeScale > 8)
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{
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simManager.timeScale = 8;
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}
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posFromPlanet *= simManager.scale;
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Vector2d currentVel = new Vector2d(currentOrbitalParams.v * Mathd.Cos(currentOrbitalParams.theta), currentOrbitalParams.v * Mathd.Sin(currentOrbitalParams.theta));
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currentVel += thrustVelocity * dir * Time.fixedDeltaTime * simManager.timeScale;
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CalculateOrbitalParams(currentVel, new Vector2d(posFromPlanet.x, posFromPlanet.y), orbitedPlanetScript.mass, false);
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rb.velocity = new Vector2((float)currentVel.x, (float)currentVel.y) / simManager.scale;
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}
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else
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{
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//print((new Vector2((float)dir.x, (float)dir.y) * (thrustVelocity * simManager.timeScale * Time.fixedDeltaTime)));
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rb.AddForce(new Vector2((float)dir.x, (float)dir.y).normalized * (50f * Time.deltaTime));
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//rb.velocity = rb.velocity + (new Vector2((float)dir.x, (float)dir.y) * (thrustVelocity * simManager.timeScale * Time.fixedDeltaTime))/simManager.scale;
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Vector2d currentVel = new Vector2d(rb.velocity.x, rb.velocity.y) * simManager.scale;
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Vector2 posFromPlanet = (Vector2)transform.position - (Vector2) orbitedPlanet.position;
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posFromPlanet *= simManager.scale;
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CalculateOrbitalParams(currentVel, new Vector2d(posFromPlanet.x, posFromPlanet.y), orbitedPlanetScript.mass, false);
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}
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}
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if (Vector2.Distance(transform.position, orbitedPlanet.position) > (orbitedPlanetScript.radius + physicsDistance)/simManager.scale)
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{
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rb.isKinematic = true;
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Vector2d pos = currentOrbitalParams.RecalculateAtTime(simManager.time);
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Vector3 relative = new Vector3((float) pos.x / simManager.scale, (float) pos.y / simManager.scale, 0f);
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shipToPlanetLR.positionCount = 2;
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perpRLR.positionCount = 2;
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shipToPlanetLR.SetPositions(new Vector3[]{new Vector3(0f,0f,0f), relative});
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perpRLR.SetPositions(new Vector3[]{relative, relative + new Vector3((float)dir.x, (float)dir.y) * 500f});
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float velAngle = (float) currentOrbitalParams.theta;
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float vel = (float) currentOrbitalParams.v;
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Vector3 velocityVector = new Vector3(vel * Mathf.Cos(velAngle), vel * Mathf.Sin(velAngle));
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velocityLR.SetPositions(new Vector3[]{relative, velocityVector + relative});
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transform.position = orbitedPlanet.position + relative;
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Vector2d currentVel = new Vector2d(currentOrbitalParams.v * Mathd.Cos(currentOrbitalParams.theta), currentOrbitalParams.v * Mathd.Sin(currentOrbitalParams.theta));
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rb.velocity = new Vector2((float)currentVel.x, (float)currentVel.y) / simManager.scale;
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}
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else
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{
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if (simManager.timeScale > 4)
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{
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simManager.timeScale = 4;
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}
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rb.isKinematic = false;
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double gravVal = currentOrbitalParams.G *
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(orbitedPlanetScript.mass /
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Mathf.Pow(Vector2.Distance(orbitedPlanet.position, transform.position) * simManager.scale,
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2));
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print(gravVal);
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print((float)gravVal * Time.fixedDeltaTime * (10/simManager.scale));
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rb.velocity = rb.velocity + (float) gravVal * (1 / simManager.scale) * Time.fixedDeltaTime * simManager.timeScale *
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(Vector2)(orbitedPlanet.position - transform.position).normalized;
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//rb.AddForce(((float)gravVal * rb.mass * (10/simManager.scale) * Time.fixedDeltaTime * simManager.timeScale * (orbitedPlanet.position - transform.position).normalized) );
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currentOrbitalParams.v = ((double) rb.velocity.magnitude * Mathd.Sign((double) rb.velocity.magnitude)) *
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simManager.scale;
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currentOrbitalParams.theta = Mathd.Atan2(rb.velocity.normalized.y, rb.velocity.normalized.x);
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}
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}
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private void LateUpdate()
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{
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orbitLR.transform.position = orbitedPlanet.position;
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orbitLR.transform.rotation = Quaternion.identity;
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perpRLR.transform.position = orbitedPlanet.position;
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perpRLR.transform.rotation = Quaternion.identity;
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velocityLR.transform.position = orbitedPlanet.position;
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velocityLR.transform.rotation = Quaternion.identity;
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shipToPlanetLR.transform.position = orbitedPlanet.position + new Vector3(0f, 0f, 1f);
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shipToPlanetLR.transform.rotation = Quaternion.identity;
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Camera.main.transform.rotation = Quaternion.identity;
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//RotateCam();
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}
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void CalculateOrbitalParams(Vector2d initialVel, Vector2d positionFromPlanet, double planetMass, bool doPrints)
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{
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currentOrbitalParams = new OrbitalParameters();
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currentOrbitalParams.CalculateAllInitialParams(initialVel, positionFromPlanet, planetMass, simManager.time - Time.fixedDeltaTime * simManager.timeScale, doPrints);
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DrawOrbit(100);
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}
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void DrawOrbit(int posCount)
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{
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orbitLR.positionCount = posCount;
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Vector3[] positions = new Vector3[posCount];
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for (var i = 0; i < posCount; i++)
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{
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double value;
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if (currentOrbitalParams.e < 1)
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{
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value = ((currentOrbitalParams.T / posCount) * i) + currentOrbitalParams.t0;;
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}
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else
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{
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value = ((2 * Mathd.PI / posCount) * i) + currentOrbitalParams.w;
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}
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//double dist = currentOrbitalParams.EvaluateEllipticalOrbit(currentOrbitalParams.a, currentOrbitalParams.e,
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// currentOrbitalParams.w, angle);
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//Vector2d pos = new Vector2d(dist * Mathd.Cos(angle), dist * Mathd.Sin(angle));
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Vector2d pos = currentOrbitalParams.GetPositionAtTime(value);
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Vector2 adjustedPos = new Vector2((float)pos.x/simManager.scale, (float)pos.y/simManager.scale);
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positions[i] = adjustedPos;
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}
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orbitLR.SetPositions(positions);
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}
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void ZoomOrthoCamera()
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{
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// Calculate how much we will have to move towards the zoomTowards position
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mouseScrollMultiplier = curveForMouseZoom.Evaluate(cam.orthographicSize/maxZoom) * maxMouseZoomMultiplier;
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// Zoom camera
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cam.orthographicSize -= Input.mouseScrollDelta.y * mouseScrollMultiplier;
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// Limit zoom
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cam.orthographicSize = Mathf.Clamp(cam.orthographicSize, minZoom, maxZoom);
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}
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void RotateCam()
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{
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Vector2 dir = transform.position - orbitedPlanet.position;
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float angle = Mathf.Atan2(dir.y, dir.x) * Mathf.Rad2Deg;
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angle -= 90f;
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cam.transform.rotation = Quaternion.Euler(0f, 0f, angle);
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}
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}
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[System.Serializable]
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public class OrbitalParameters
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{
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[Header("Semi-major axis")] public double a;
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[Header("Semi-minor axis")] public double b;
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[Header("Eccentricity")] public double e;
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[Header("True Anomaly")] public double f;
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[Header("Angle Of Perigee")] public double w;
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[Header("Eccentric Anomaly")] public double E;
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[Header("Initial Mean Anomaly")] public double M0;
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[Header("Initial Time")] public double t0;
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[Header("Current Mean Anomaly")] public double M;
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[Header("Orbital Period")] public double T;
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[Header("Mean Motion")] public double n;
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[Header("Flight Path Angle")] public double phi;
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[Header("Velocity")] public double v;
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[Header("VelAngle")] public double theta;
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private Vector2d eVec;
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[HideInInspector]
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public double h;
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private double u;
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[HideInInspector]
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public double G = 6.67408 * Mathd.Pow(10, -11);
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public void CalculateAllInitialParams(Vector2d velocity, Vector2d positionFromPlanet, double planetMass, double _t0, bool doPrints)
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{
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u = G * planetMass;
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t0 = _t0;
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if (doPrints)
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{
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Debug.Log("circleVel: " + Mathd.Sqrt(u/positionFromPlanet.magnitude) + ", escape Vel: " + Mathd.Sqrt(2 * u/positionFromPlanet.magnitude));
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}
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//circular vel
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//velocity = new Vector2d(-Mathd.Sqrt(u/positionFromPlanet.magnitude), 0);
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//parabolic vel - escape vel
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//velocity = new Vector2d(Mathd.Sqrt(2 * u/positionFromPlanet.magnitude), 0);
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a = CalculateSemiMajorAxis(velocity.magnitude, positionFromPlanet.magnitude, u);
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h = Vector2d.CrossProduct(positionFromPlanet, velocity);
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eVec = CalculateEccentricityVector(velocity, positionFromPlanet, u);
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e = eVec.magnitude;
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T = CalculateOrbitalPeriod(u, a, e);
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n = CalculateMeanMotion(T, h, e, u, a);
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f = TrueAnomalyFromStateVectors(eVec, positionFromPlanet, velocity);
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w = AngleOfPerigee(positionFromPlanet, f);
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if (doPrints)
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{
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Debug.Log("(" + eVec.x + ", " + eVec.y + ")");
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}
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if (e < 1)
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{
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E = CalculateEccentricAnomalyFromTrueAnomaly(f, e);
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M0 = MeanAnomalyFromEccentricAnomaly(E, e);
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M = M0;
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if (doPrints)
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{
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Debug.Log(f + " " + E);
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}
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}
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else if(e >= 1)
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{
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E = CalculateHyperbolicAnomalyFromTrueAnomaly(f, e);
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M0 = MeanAnomalyFromHyperbolicAnomaly(E, e);
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M = M0;
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if (doPrints)
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{
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Debug.Log(f + " " + E + " " + (e * Mathd.Sinh(E) - E));
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}
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}
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else
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{
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}
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v = CalculateVelocityVisViva(a, u, positionFromPlanet.magnitude);
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phi = CalculateFlightPathAngle(e, f);
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theta = GetCurrentDirectionOfVelocity(positionFromPlanet, phi, h);
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//E = CalculateEccentricAnomalyFromMeanAnomaly(e, M, 5);
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}
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//not context based
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public Vector2d GetPositionAtTime(double t)
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{
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if (e < 1)
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{
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double _M = M0 + n * (t - t0);
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double _E = CalculateEccentricAnomalyFromMeanAnomaly(e, _M, 7);
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double _f = CalculateTrueAnomalyFromEccentricAnomaly(_E, e, 7);
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double angle = _f + w;
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double r = EvaluateOrbit(a, e, w, angle);
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return new Vector2d(r * Mathd.Cos(angle),r * Mathd.Sin(angle));
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}
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else
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{
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/*double _M = M0 + n * (t - t0);
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double _E = CalculateHyperbolicAnomalyFromMeanAnomaly(e, _M, 7);
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double _f = CalculateTrueAnomalyFromHyperbolicAnomaly(_E, e);
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double angle = _f + w;
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double r = EvaluateOrbit(a, e, w, angle);
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return new Vector2d(r * Mathd.Cos(angle),r * Mathd.Sin(angle));*/
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double r = EvaluateOrbit(a, e, w, t);
|
|
||||||
return new Vector2d(r * Mathd.Cos(t), r * Mathd.Sin(t));
|
|
||||||
}
|
|
||||||
|
|
||||||
}
|
|
||||||
|
|
||||||
//context based
|
|
||||||
public Vector2d RecalculateAtTime(double t)
|
|
||||||
{
|
|
||||||
if (e < 1)
|
|
||||||
{
|
|
||||||
M = M0 + n * (t - t0);
|
|
||||||
E = CalculateEccentricAnomalyFromMeanAnomaly(e, M, 7);
|
|
||||||
f = CalculateTrueAnomalyFromEccentricAnomaly(E, e, 7);
|
|
||||||
double angle = f + w;
|
|
||||||
double r = EvaluateOrbit(a, e, w, angle);
|
|
||||||
Vector2d pos = new Vector2d(r * Mathd.Cos(angle),r * Mathd.Sin(angle));
|
|
||||||
v = CalculateVelocityVisViva(a, u, pos.magnitude);
|
|
||||||
phi = CalculateFlightPathAngle(e, f);
|
|
||||||
theta = GetCurrentDirectionOfVelocity(pos, phi,h);
|
|
||||||
return pos;
|
|
||||||
}
|
|
||||||
else
|
|
||||||
{
|
|
||||||
M = M0 + n * (t - t0);
|
|
||||||
E = CalculateHyperbolicAnomalyFromMeanAnomaly(e, M, 7);
|
|
||||||
f = CalculateTrueAnomalyFromHyperbolicAnomaly(E, e);
|
|
||||||
double angle = f + w;
|
|
||||||
double r = EvaluateOrbit(a, e, w, angle);
|
|
||||||
Vector2d pos = new Vector2d(r * Mathd.Cos(angle),r * Mathd.Sin(angle));
|
|
||||||
v = CalculateVelocityVisViva(a, u, pos.magnitude);
|
|
||||||
phi = CalculateFlightPathAngle(e, f);
|
|
||||||
theta = GetCurrentDirectionOfVelocity(pos, phi, h);
|
|
||||||
return pos;
|
|
||||||
}
|
|
||||||
}
|
|
||||||
|
|
||||||
public double EvaluateOrbit(double _a, double _e, double _w, double angle)
|
|
||||||
{
|
|
||||||
double top = _a * (1 - Mathd.Pow(_e, 2));
|
|
||||||
double bot = 1 + e * Mathd.Cos(angle - _w);
|
|
||||||
return top / bot;
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateVelocityVisViva(double _a, double _u, double _r)
|
|
||||||
{
|
|
||||||
return Mathd.Sqrt(_u * ((2.0 / _r) - (1.0 / _a)));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateFlightPathAngle(double _e, double _f)
|
|
||||||
{
|
|
||||||
return Mathd.Atan2(_e * Mathd.Sin(_f), 1 + _e * Mathd.Cos(_f));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double GetCurrentDirectionOfVelocity(Vector2d pos, double _phi, double _h)
|
|
||||||
{
|
|
||||||
Vector2d perp = new Vector2d(pos.y, -pos.x) * 0.5f;
|
|
||||||
Vector2d perp2 = new Vector2d(-pos.y, pos.x) * 0.5f;
|
|
||||||
double perpAngle = Mathd.Atan2(perp2.y - perp.y, perp2.x - perp.x);
|
|
||||||
double velAngle;
|
|
||||||
if (_h < 0)
|
|
||||||
{
|
|
||||||
velAngle = perpAngle - _phi + Mathd.PI;
|
|
||||||
}
|
|
||||||
else
|
|
||||||
{
|
|
||||||
velAngle = perpAngle - _phi;
|
|
||||||
}
|
|
||||||
|
|
||||||
return velAngle;
|
|
||||||
}
|
|
||||||
|
|
||||||
public double AngleOfPerigee(Vector2d r, double _f)
|
|
||||||
{
|
|
||||||
return Mathd.Atan2(r.y, r.x) - _f;
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateSemiMajorAxis(double v, double r, double u)
|
|
||||||
{
|
|
||||||
return (u * r) / (2 * u - (Mathd.Pow(v, 2) * r));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateOrbitalPeriod(double u, double _a, double _e)
|
|
||||||
{
|
|
||||||
if (_e <= 1)
|
|
||||||
{
|
|
||||||
return 2 * Mathd.PI * Mathd.Sqrt(Mathd.Pow(_a, 3) / u);
|
|
||||||
}
|
|
||||||
else
|
|
||||||
{
|
|
||||||
return -1;
|
|
||||||
}
|
|
||||||
}
|
|
||||||
|
|
||||||
//WRONG GIVES MEAN MOTION U IDIOT MF.
|
|
||||||
public double CalculateMeanMotion(double _T, double _h, double _e, double _u, double _a)
|
|
||||||
{
|
|
||||||
if (_e < 1)
|
|
||||||
{
|
|
||||||
return (2 * Mathd.PI) / _T * Mathd.Sign(_h);
|
|
||||||
}
|
|
||||||
else if (_e > 1)
|
|
||||||
{
|
|
||||||
return Mathd.Sqrt(_u / -Mathd.Pow(_a, 3)) * Mathd.Sign(_h);
|
|
||||||
}
|
|
||||||
else
|
|
||||||
{
|
|
||||||
return Mathd.Sqrt(_u / Mathd.Pow(_a, 3)) * Mathd.Sign(_h);
|
|
||||||
}
|
|
||||||
|
|
||||||
}
|
|
||||||
|
|
||||||
public Vector2d CalculateEccentricityVector(Vector2d v, Vector2d r, double u)
|
|
||||||
{
|
|
||||||
double _h = Vector2d.CrossProduct(r, v);
|
|
||||||
return ((Mathd.Pow(v.magnitude, 2) - (u / r.magnitude)) * r - Vector2d.Dot(r, v) * v) / u;
|
|
||||||
//return new Vector2d(((v.y * _h)/u) - (r.x/r.magnitude), ((v.x * _h)/u) - (r.y/r.magnitude));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateEccentricAnomalyFromMeanAnomaly(double _e, double _M, int dp)
|
|
||||||
{
|
|
||||||
//dp = number of decimal places
|
|
||||||
|
|
||||||
int maxIter=30, i=0;
|
|
||||||
|
|
||||||
double delta=Mathd.Pow(10,-dp);
|
|
||||||
|
|
||||||
double _E, F;
|
|
||||||
|
|
||||||
_E=_M;
|
|
||||||
|
|
||||||
F = _E - _e*Mathd.Sin(_M) - _M;
|
|
||||||
|
|
||||||
while ((Mathd.Abs(F)>delta) && (i<maxIter)) {
|
|
||||||
|
|
||||||
_E = _E - F/(1.0-_e*Mathd.Cos(_E));
|
|
||||||
F = _E - _e*Math.Sin(_E) - _M;
|
|
||||||
|
|
||||||
i = i + 1;
|
|
||||||
|
|
||||||
}
|
|
||||||
|
|
||||||
return _E;
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateHyperbolicAnomalyFromMeanAnomaly(double _e, double _M, int dp)
|
|
||||||
{
|
|
||||||
//dp = number of decimal places
|
|
||||||
|
|
||||||
int maxIter=30, i=0;
|
|
||||||
|
|
||||||
double delta=Mathd.Pow(10,-dp);
|
|
||||||
|
|
||||||
double _E, F;
|
|
||||||
|
|
||||||
_E=_M;
|
|
||||||
|
|
||||||
F = _e * Mathd.Sinh(_E) - _E - _M;
|
|
||||||
|
|
||||||
while ((Mathd.Abs(F)>delta) && (i<maxIter)) {
|
|
||||||
|
|
||||||
_E = _E + F/(1.0 - _e * Mathd.Cosh(_E));
|
|
||||||
F = _e * Mathd.Sinh(_E) - _E - _M;
|
|
||||||
|
|
||||||
i = i + 1;
|
|
||||||
|
|
||||||
}
|
|
||||||
|
|
||||||
return _E;
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateEccentricAnomalyFromTrueAnomaly(double _f, double _e)
|
|
||||||
{
|
|
||||||
return Mathd.Atan2(Mathd.Sqrt(1 - Mathd.Pow(_e, 2)) * Mathd.Sin(_f), _e + Mathd.Cos(_f));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateHyperbolicAnomalyFromTrueAnomaly(double _f, double _e)
|
|
||||||
{
|
|
||||||
return 2 * Mathd.Atanh(Mathd.Sqrt((_e - 1)/(_e + 1)) * Mathd.Tan(_f/2));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double MeanAnomalyFromEccentricAnomaly(double _E, double _e)
|
|
||||||
{
|
|
||||||
return _E - _e * Mathd.Sin(_E);
|
|
||||||
}
|
|
||||||
|
|
||||||
public double MeanAnomalyFromHyperbolicAnomaly(double _H, double _e)
|
|
||||||
{
|
|
||||||
return _e * Mathd.Sinh(_H) - _H;
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateTrueAnomalyFromEccentricAnomaly(double _E, double _e, int dp)
|
|
||||||
{
|
|
||||||
return Mathd.Atan2(Mathd.Sqrt(1 - Mathd.Pow(_e, 2)) * Mathd.Sin(_E), Mathd.Cos(_E) - _e);
|
|
||||||
}
|
|
||||||
|
|
||||||
public double CalculateTrueAnomalyFromHyperbolicAnomaly(double _H, double _e)
|
|
||||||
{
|
|
||||||
return 2 * Mathd.Atan2(Mathd.Sqrt(_e + 1) * Mathd.Sinh(_H/2), Mathd.Sqrt(_e - 1) * Mathd.Cosh(_H/2));
|
|
||||||
}
|
|
||||||
|
|
||||||
public double TrueAnomalyFromStateVectors(Vector2d _e, Vector2d r, Vector2d v)
|
|
||||||
{
|
|
||||||
if (_e.magnitude > 0)
|
|
||||||
{
|
|
||||||
double h = Vector2d.CrossProduct(r, v);
|
|
||||||
double val = Mathd.Acos(Vector2d.Dot(_e, r) / (_e.magnitude * r.magnitude));
|
|
||||||
if (!Mathd.Approximately(Mathd.Sign(Vector2d.Dot(r, v)), Mathd.Sign(h)))
|
|
||||||
{
|
|
||||||
return (2 * Mathd.PI) - val;
|
|
||||||
}
|
|
||||||
else
|
|
||||||
{
|
|
||||||
return val;
|
|
||||||
}
|
|
||||||
}
|
|
||||||
else
|
|
||||||
{
|
|
||||||
return Mathd.Atan2(r.y, r.x);
|
|
||||||
}
|
|
||||||
|
|
||||||
}
|
|
||||||
|
|
||||||
}
|
|
||||||
Loading…
Reference in New Issue