254 lines
6.7 KiB
Text
254 lines
6.7 KiB
Text
###########################################################################
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# simulation of a faraway orbital target (needs handover to spacecraft-specific
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# code for close range)
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# Thorsten Renk 2016-2019
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###########################################################################
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var orbitalTarget = {
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new: func(altitude, inclination, node_longitude, anomaly) {
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var t = { parents: [orbitalTarget] };
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t.altitude = altitude;
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t.radius = 20908323.0 * 0.3048 + t.altitude;
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t.GM = 398759391386476.0;
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#t.GM = 398600441800000.0;
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t.period = 2.0 * math.pi * math.sqrt(math.pow(t.radius, 3.0)/ t.GM);
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t.inclination = inclination;
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t.inc_rad = t.inclination * math.pi/180.0;
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t.l_vec = [math.sin(t.inc_rad), 0.0, math.cos(t.inc_rad)];
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t.node_longitude = node_longitude;
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t.nl_rad = t.node_longitude * math.pi/180.0;
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t.initial_nl_rad = t.nl_rad;
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var l_tmp = t.l_vec[0];
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t.l_vec[0] = math.sin(t.nl_rad) * l_tmp;
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t.l_vec[1] = -math.cos(t.nl_rad) * l_tmp;
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t.anomaly = anomaly;
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t.anomaly_rad = t.anomaly * math.pi/180.0;
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t.initial_anomaly_rad = t.anomaly_rad;
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t.delta_lon = 0.0;
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t.update_time = 0.1;
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t.running_flag = 0;
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t.elapsed_time = 0.0;
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t.delta_time = 0.0;
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t.label = "";
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# Coefficients for the J3 altitude variation
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var inc_var = t.inclination/60.0;
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#print ("inc_var:", inc_var);
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t.coeff1 = (10268. - 0.99579 * (t.altitude / 1000.0)) * inc_var;
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t.coeff2 = 0.212 * 2.0 * math.pi;
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#t.node_drift = -4361.26 * 1./math.pow(t.radius/1000.0 ,2.0) * math.cos(t.inc_rad);
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t.node_drift = -2.16732e+9 /math.pow(t.radius/1000.0, 3.48908) * math.cos(t.inc_rad);
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print ("Drift rate: ", t.node_drift);
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return t;
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},
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set_anomaly: func (anomaly) {
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t.anomaly = anomaly;
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t.anomaly_rad = t.anomaly * math.pi/180.0;
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},
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set_delta_lon: func (dl) {
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t.delta_lon = dl;
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},
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list: func {
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print("Radius: ", me.radius, " period: ", me.period);
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print("L_vector: ", me.l_vec[0], " ", me.l_vec[1], " ", me.l_vec[2]);
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print("L_norm: ", math.sqrt(me.l_vec[0] * me.l_vec[0] + me.l_vec[1] * me.l_vec[1] + me.l_vec[2] * me.l_vec[2]));
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var pos = me.get_inertial_pos();
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print("Inertial: ", pos[0], " ", pos[1], " ", pos[2]);
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print("Rad: ", math.sqrt(pos[0] * pos[0] + pos[1] * pos[1] + pos[2] * pos[2]));
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var lla = me.get_latlonalt();
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print("Lat: ", lla[0], " lon: ", lla[1], " alt: ", lla[2]);
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},
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evolve: func {
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var dt = getprop("/sim/time/delta-sec");
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#var speedup = getprop("/sim/speed-up");
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#dt = dt * speedup;
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me.anomaly_rad = me.anomaly_rad + dt/me.period * 2.0 * math.pi;
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if (me.anomaly_rad > 2.0 * math.pi)
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{
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me.anomaly_rad = me.anomaly_rad - 2.0 * math.pi;
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}
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me.anomaly = me.anomaly_rad * 180.0/math.pi;
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me.delta_lon = me.delta_lon + dt * 0.00418333333333327;
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me.node_longitude = me.node_longitude + me.node_drift * dt;
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me.nl_rad = me.node_longitude * math.pi/180.0;
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me.l_vec = [math.sin(me.inc_rad), 0.0, math.cos(me.inc_rad)];
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var l_tmp = me.l_vec[0];
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me.l_vec[0] = math.sin(me.nl_rad) * l_tmp;
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me.l_vec[1] = -math.cos(me.nl_rad) * l_tmp;
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},
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get_inertial_pos: func {
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return me.compute_inertial_pos(me.anomaly_rad, me.nl_rad);
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},
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get_inertial_pos_at_time: func (time) {
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var anomaly_rad = me.initial_anomaly_rad + (time - me.delta_time)/me.period * 2.0 * math.pi;
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while (anomaly_rad > 2.0 * math.pi)
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{
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anomaly_rad = anomaly_rad - 2.0 * math.pi;
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}
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var nl_rad = me.initial_nl_rad + me.node_drift * (time - me.delta_time) * math.pi/180.0;
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return me.compute_inertial_pos(anomaly_rad, nl_rad);
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},
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get_inertial_speed: func () {
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# obtain via numerical discretization from two points
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var anomaly_rad = me.anomaly_rad;
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while (anomaly_rad > 2.0 * math.pi)
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{
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anomaly_rad = anomaly_rad - 2.0 * math.pi;
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}
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var pos1 = me.compute_inertial_pos(anomaly_rad, me.nl_rad);
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anomaly_rad = me.anomaly_rad + 0.1/me.period * 2.0 * math.pi;
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while (anomaly_rad > 2.0 * math.pi)
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{
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anomaly_rad = anomaly_rad - 2.0 * math.pi;
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}
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var pos2 = me.compute_inertial_pos(anomaly_rad, me.nl_rad);
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var vx = (pos2[0] - pos1[0])/0.1;
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var vy = (pos2[1] - pos1[1])/0.1;
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var vz = (pos2[2] - pos1[2])/0.1;
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return [vx, vy, vz];
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},
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get_inertial_speed_at_time: func (time) {
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# obtain via numerical discretization from two points
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var anomaly_rad = me.initial_anomaly_rad + (time- me.delta_time)/me.period * 2.0 * math.pi;
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while (anomaly_rad > 2.0 * math.pi)
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{
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anomaly_rad = anomaly_rad - 2.0 * math.pi;
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}
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var nl_rad = me.initial_nl_rad + me.node_drift * (time - me.delta_time) * math.pi/180.0;
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var pos1 = me.compute_inertial_pos(anomaly_rad, nl_rad);
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anomaly_rad = me.initial_anomaly_rad + ((time - me.delta_time) + 0.1)/me.period * 2.0 * math.pi;
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while (anomaly_rad > 2.0 * math.pi)
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{
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anomaly_rad = anomaly_rad - 2.0 * math.pi;
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}
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nl_rad = me.initial_nl_rad + me.node_drift * ((time - me.delta_time) +0.1) * math.pi/180.0;
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var pos2 = me.compute_inertial_pos(anomaly_rad, nl_rad);
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var vx = (pos2[0] - pos1[0])/0.1;
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var vy = (pos2[1] - pos1[1])/0.1;
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var vz = (pos2[2] - pos1[2])/0.1;
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return [vx, vy, vz];
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},
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compute_inertial_pos: func (anomaly_rad, nl_rad) {
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# J3 variation around radius
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while (anomaly_rad > 2.0 * math.pi)
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{
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anomaly_rad = anomaly_rad - 2.0 * math.pi;
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}
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while (anomaly_rad < 0.0)
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{
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anomaly_rad = anomaly_rad + 2.0 * math.pi;
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}
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var r_corr = me.coeff1 * math.exp(- math.pow(((anomaly_rad - math.pi)/ me.coeff2),2.0));
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#print (r_corr);
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# movement around equatorial orbit
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var x = (me.radius + r_corr) * math.cos(anomaly_rad);
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var y = (me.radius + r_corr) * math.sin(anomaly_rad);
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var z = 0;
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# tilt with inclination
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z = y * math.sin(me.inc_rad);
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y = y * math.cos(me.inc_rad);
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# rotate with node longitude
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var xp = x * math.cos(nl_rad) - y * math.sin(nl_rad);
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var yp = x * math.sin(nl_rad) + y * math.cos(nl_rad);
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# this is a good bit of trickery to capture leading J3 dynamics
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var corr_200 = -2.6e-5 * me.inclination + 1.00321;
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var corr = corr_200 * (1.0 + (me.altitude/1000.0-200.0) * 6e-7);
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corr = 1.0 + (0.64 * (corr -1.0));
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#print ("Corr200 is now:", corr_200);
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#print ("Corr is now:", corr);
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#print ("Altitude: ", me.altitude);
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z /= corr;
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return [xp, yp, z];
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},
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get_latlonalt: func {
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var coordinates = geo.Coord.new();
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var inertial_pos = me.get_inertial_pos();
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coordinates.set_xyz(inertial_pos[0], inertial_pos[1], inertial_pos[2]);
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coordinates.set_lon(coordinates.lon() - me.delta_lon);
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return [coordinates.lat(), coordinates.lon(), coordinates.alt()];
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},
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start: func {
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if (me.running_flag == 1) {return;}
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me.running_flag = 1;
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me.run();
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},
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stop: func {
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me.running_flag = 0;
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},
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run: func {
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me.evolve (me.update_time);
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if (me.running_flag == 1)
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{settimer(func me.run(), 0);}
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},
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};
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