Source code for EXOSIMS.SurveySimulation.linearJScheduler_det_only

from EXOSIMS.SurveySimulation.linearJScheduler import linearJScheduler
import astropy.units as u
import numpy as np
import time
import astropy.constants as const
from EXOSIMS.util._numpy_compat import copy_if_needed


[docs] class linearJScheduler_det_only(linearJScheduler): """linearJScheduler_det_only - linearJScheduler Detections Only This class implements the linear cost function scheduler described in Savransky et al. (2010). This scheduler inherits from the linearJScheduler module but performs only detections. Args: specs: user specified values """ def __init__(self, **specs): linearJScheduler.__init__(self, **specs)
[docs] def run_sim(self): """Performs the survey simulation""" OS = self.OpticalSystem TL = self.TargetList SU = self.SimulatedUniverse Obs = self.Observatory TK = self.TimeKeeping # TODO: start using this self.currentSep # set occulter separation if haveOcculter if OS.haveOcculter: self.currentSep = Obs.occulterSep # choose observing modes selected for detection (default marked with a flag) allModes = OS.observingModes det_mode = list(filter(lambda mode: mode["detectionMode"], allModes))[0] # begin Survey, and loop until mission is finished log_begin = "OB%s: survey beginning." % (TK.OBnumber) self.logger.info(log_begin) self.vprint(log_begin) t0 = time.time() sInd = None ObsNum = 0 while not TK.mission_is_over(OS, Obs, det_mode): # acquire the NEXT TARGET star index and create DRM old_sInd = sInd # used to save sInd if returned sInd is None DRM, sInd, det_intTime, waitTime = self.next_target(sInd, det_mode) if sInd is not None: ObsNum += ( 1 # we're making an observation so increment observation number ) if OS.haveOcculter: # advance to start of observation # (add slew time for selected target) _ = TK.advanceToAbsTime(TK.currentTimeAbs.copy() + waitTime) # beginning of observation, start to populate DRM DRM["star_ind"] = sInd DRM["star_name"] = TL.Name[sInd] DRM["arrival_time"] = TK.currentTimeNorm.to("day").copy() DRM["OB_nb"] = TK.OBnumber DRM["ObsNum"] = ObsNum pInds = np.where(SU.plan2star == sInd)[0] DRM["plan_inds"] = pInds.astype(int) log_obs = ( " Observation #%s, star ind %s (of %s) with %s planet(s), " + "mission time at Obs start: %s" ) % ( ObsNum, sInd, TL.nStars, len(pInds), TK.currentTimeNorm.to("day").copy().round(2), ) self.logger.info(log_obs) self.vprint(log_obs) # PERFORM DETECTION and populate revisit list attribute ( detected, det_fZ, det_JEZ, det_systemParams, det_SNR, FA, ) = self.observation_detection(sInd, det_intTime, det_mode) # update the occulter wet mass if OS.haveOcculter: DRM = self.update_occulter_mass(DRM, sInd, det_intTime, "det") # populate the DRM with detection results DRM["det_time"] = det_intTime.to("day") DRM["det_status"] = detected DRM["det_SNR"] = det_SNR DRM["det_fZ"] = det_fZ.to("1/arcsec2") DRM["det_params"] = det_systemParams # populate the DRM with observation modes DRM["det_mode"] = dict(det_mode) del DRM["det_mode"]["inst"], DRM["det_mode"]["syst"] DRM["exoplanetObsTime"] = TK.exoplanetObsTime.copy() # append result values to self.DRM self.DRM.append(DRM) # handle case of inf OBs and missionPortion < 1 if np.isinf(TK.OBduration) and (TK.missionPortion < 1): self.arbitrary_time_advancement( TK.currentTimeNorm.to("day").copy() - DRM["arrival_time"] ) else: # sInd == None sInd = old_sInd # Retain the last observed star if ( TK.currentTimeNorm.copy() >= TK.OBendTimes[TK.OBnumber] ): # currentTime is at end of OB # Conditional Advance To Start of Next OB if not TK.mission_is_over( OS, Obs, det_mode ): # as long as the mission is not over TK.advancetToStartOfNextOB() # Advance To Start of Next OB elif waitTime is not None: # CASE 1: Advance specific wait time _ = TK.advanceToAbsTime(TK.currentTimeAbs.copy() + waitTime) self.vprint("waitTime is not None") else: startTimes = ( TK.currentTimeAbs.copy() + np.zeros(TL.nStars) * u.d ) # Start Times of Observations observableTimes = Obs.calculate_observableTimes( TL, np.arange(TL.nStars), startTimes, self.koMap, self.koTimes, det_mode, )[0] # CASE 2 If There are no observable targets for the rest # of the mission if ( observableTimes[ ( TK.missionFinishAbs.copy().value * u.d > observableTimes.value * u.d ) * ( observableTimes.value * u.d >= TK.currentTimeAbs.copy().value * u.d ) ].shape[0] ) == 0: self.vprint( ( "No Observable Targets for Remainder of mission at " "currentTimeNorm = {}" ).format(TK.currentTimeNorm) ) # Manually advancing time to mission end TK.currentTimeNorm = TK.missionLife TK.currentTimeAbs = TK.missionFinishAbs else: # CASE 3 nominal wait time if at least 1 target is still # in list and observable # TODO: ADD ADVANCE TO WHEN FZMIN OCURS inds1 = np.arange(TL.nStars)[ observableTimes.value * u.d > TK.currentTimeAbs.copy().value * u.d ] # apply intTime filter inds2 = np.intersect1d(self.intTimeFilterInds, inds1) # apply revisit Filter #NOTE this means stars you added # to the revisit list inds3 = self.revisitFilter( inds2, TK.currentTimeNorm.copy() + self.dt_max.to(u.d) ) self.vprint( "Filtering %d stars from advanceToAbsTime" % (TL.nStars - len(inds3)) ) oTnowToEnd = observableTimes[inds3] # there is at least one observableTime between now and the # end of the mission if not oTnowToEnd.value.shape[0] == 0: tAbs = np.min(oTnowToEnd) # advance to that observable time else: # advance to end of mission tAbs = TK.missionStart + TK.missionLife tmpcurrentTimeNorm = TK.currentTimeNorm.copy() # Advance Time to this time OR start of next OB following # this time _ = TK.advanceToAbsTime(tAbs) self.vprint( ( "No Observable Targets a currentTimeNorm= {:.2f} " "Advanced To currentTimeNorm= {:.2f}" ).format( tmpcurrentTimeNorm.to("day"), TK.currentTimeNorm.to("day"), ) ) else: # TK.mission_is_over() dtsim = (time.time() - t0) * u.s log_end = ( "Mission complete: no more time available.\n" + "Simulation duration: %s.\n" % dtsim.astype("int") + "Results stored in SurveySimulation.DRM (Design Reference Mission)." ) self.logger.info(log_end) print(log_end)
[docs] def next_target(self, old_sInd, mode): """Finds index of next target star and calculates its integration time. This method chooses the next target star index based on which stars are available, their integration time, and maximum completeness. Returns None if no target could be found. Args: old_sInd (integer): Index of the previous target star mode (dict): Selected observing mode for detection Returns: tuple: DRM (dict): Design Reference Mission, contains the results of one complete observation (detection and characterization) sInd (integer): Index of next target star. Defaults to None. intTime (astropy Quantity): Selected star integration time for detection in units of day. Defaults to None. waitTime (astropy Quantity): a strategically advantageous amount of time to wait in the case of an occulter for slew times """ OS = self.OpticalSystem TL = self.TargetList Obs = self.Observatory TK = self.TimeKeeping # create DRM DRM = {} # selecting appropriate koMap koMap = self.koMaps[mode["syst"]["name"]] # allocate settling time + overhead time tmpCurrentTimeAbs = ( TK.currentTimeAbs.copy() + Obs.settlingTime + mode["syst"]["ohTime"] ) tmpCurrentTimeNorm = ( TK.currentTimeNorm.copy() + Obs.settlingTime + mode["syst"]["ohTime"] ) # look for available targets # 1. initialize arrays slewTimes = np.zeros(TL.nStars) * u.d # fZs = np.zeros(TL.nStars) / u.arcsec**2 dV = np.zeros(TL.nStars) * u.m / u.s intTimes = np.zeros(TL.nStars) * u.d obsTimes = np.zeros([2, TL.nStars]) * u.d sInds = np.arange(TL.nStars) # 2. find spacecraft orbital START positions (if occulter, positions # differ for each star) and filter out unavailable targets sd = None if OS.haveOcculter: sd = Obs.star_angularSep(TL, old_sInd, sInds, tmpCurrentTimeAbs) obsTimes = Obs.calculate_observableTimes( TL, sInds, tmpCurrentTimeAbs, self.koMaps, self.koTimes, mode ) slewTimes = Obs.calculate_slewTimes( TL, old_sInd, sInds, sd, obsTimes, tmpCurrentTimeAbs ) # 2.1 filter out totTimes > integration cutoff if len(sInds.tolist()) > 0: sInds = np.intersect1d(self.intTimeFilterInds, sInds) # start times, including slew times startTimes = tmpCurrentTimeAbs.copy() + slewTimes startTimesNorm = tmpCurrentTimeNorm.copy() + slewTimes # 2.5 Filter stars not observable at startTimes try: koTimeInd = np.where( np.round(startTimes[0].value) - self.koTimes.value == 0 )[0][ 0 ] # find indice where koTime is startTime[0] sInds = sInds[ np.where(np.transpose(koMap)[koTimeInd].astype(bool)[sInds])[0] ] # filters inds by koMap #verified against v1.35 except: # noqa: E722 If there are no target stars to observe sInds = np.asarray([], dtype=int) # 3. filter out all previously (more-)visited targets, unless in if len(sInds.tolist()) > 0: sInds = self.revisitFilter(sInds, tmpCurrentTimeNorm) # 4.1 calculate integration times for ALL preselected targets ( maxIntTimeOBendTime, maxIntTimeExoplanetObsTime, maxIntTimeMissionLife, ) = TK.get_ObsDetectionMaxIntTime(Obs, mode) maxIntTime = min( maxIntTimeOBendTime, maxIntTimeExoplanetObsTime, maxIntTimeMissionLife ) # Maximum intTime allowed if len(sInds.tolist()) > 0: intTimes[sInds] = self.calc_targ_intTime(sInds, startTimes[sInds], mode) sInds = sInds[ np.where(intTimes[sInds] <= maxIntTime) ] # Filters targets exceeding end of OB endTimes = startTimes + intTimes if maxIntTime.value <= 0: sInds = np.asarray([], dtype=int) # 5.1 TODO Add filter to filter out stars entering and exiting keepout # between startTimes and endTimes # 5.2 find spacecraft orbital END positions (for each candidate target), # and filter out unavailable targets if len(sInds.tolist()) > 0 and Obs.checkKeepoutEnd: try: # endTimes may exist past koTimes so we have an exception to # handle this case # koTimeInd[0][0] # find indice where koTime is endTime[0] koTimeInd = np.where( np.round(endTimes[0].value) - self.koTimes.value == 0 )[0][0] # filters inds by koMap #verified against v1.35 sInds = sInds[ np.where(np.transpose(koMap)[koTimeInd].astype(bool)[sInds])[0] ] except: # noqa: E722 sInds = np.asarray([], dtype=int) # 6. choose best target from remaining if len(sInds.tolist()) > 0: # choose sInd of next target sInd, waitTime = self.choose_next_target( old_sInd, sInds, slewTimes, intTimes[sInds] ) # Should Choose Next Target decide there are no stars it wishes to # observe at this time. if (sInd is None) and (waitTime is not None): self.vprint( ( "There are no stars Choose Next Target would like to Observe. " "Waiting {}" ).format(waitTime) ) return DRM, None, None, waitTime elif (sInd is None) and (waitTime is not None): self.vprint( ( "There are no stars Choose Next Target would like to Observe " "and waitTime is None" ) ) return DRM, None, None, waitTime # store selected star integration time intTime = intTimes[sInd] # if no observable target, advanceTime to next Observable Target else: self.vprint( "No Observable Targets at currentTimeNorm= " + str(TK.currentTimeNorm.copy()) ) return DRM, None, None, None # update visited list for selected star self.starVisits[sInd] += 1 # store normalized start time for future completeness update self.lastObsTimes[sInd] = startTimesNorm[sInd] # populate DRM with occulter related values if OS.haveOcculter: DRM = Obs.log_occulterResults( DRM, slewTimes[sInd], sInd, sd[sInd], dV[sInd] ) return DRM, sInd, intTime, slewTimes[sInd] return DRM, sInd, intTime, waitTime
[docs] def choose_next_target(self, old_sInd, sInds, slewTimes, intTimes): """Choose next target based on truncated depth first search of linear cost function. Args: old_sInd (integer): Index of the previous target star sInds (integer array): Indices of available targets slewTimes (astropy quantity array): slew times to all stars (must be indexed by sInds) intTimes (astropy Quantity array): Integration times for detection in units of day Returns: sInd (integer): Index of next target star """ Comp = self.Completeness TL = self.TargetList TK = self.TimeKeeping OS = self.OpticalSystem Obs = self.Observatory allModes = OS.observingModes # cast sInds to array sInds = np.array(sInds, ndmin=1, copy=copy_if_needed) # current star has to be in the adjmat if (old_sInd is not None) and (old_sInd not in sInds): sInds = np.append(sInds, old_sInd) # calculate dt since previous observation dt = TK.currentTimeNorm + slewTimes[sInds] - self.lastObsTimes[sInds] # get dynamic completeness values comps = Comp.completeness_update(TL, sInds, self.starVisits[sInds], dt) # if first target, or if only 1 available target, # choose highest available completeness nStars = len(sInds) if (old_sInd is None) or (nStars == 1): sInd = np.random.choice(sInds[comps == max(comps)]) return sInd, slewTimes[sInd] # define adjacency matrix A = np.zeros((nStars, nStars)) # only consider slew distance when there's an occulter if OS.haveOcculter: r_ts = TL.starprop(sInds, TK.currentTimeAbs) u_ts = ( r_ts.to("AU").value.T / np.linalg.norm(r_ts.to("AU").value, axis=1) ).T angdists = np.arccos(np.clip(np.dot(u_ts, u_ts.T), -1, 1)) A[np.ones((nStars), dtype=bool)] = angdists A = self.coeffs[0] * (A) / np.pi # add factor due to completeness A = A + self.coeffs[1] * (1 - comps) # add factor due to unvisited ramp f_uv = np.zeros(nStars) unvisited = self.starVisits[sInds] == 0 f_uv[unvisited] = float(TK.currentTimeNorm.copy() / TK.missionLife.copy()) ** 2 A = A - self.coeffs[2] * f_uv # add factor due to revisited ramp f2_uv = 1 - (np.isin(sInds, self.starRevisit[:, 0])) A = A + self.coeffs[3] * f2_uv # kill diagonal A = A + np.diag(np.ones(nStars) * np.inf) # take two traversal steps step1 = np.tile(A[sInds == old_sInd, :], (nStars, 1)).flatten("F") step2 = A[np.array(np.ones((nStars, nStars)), dtype=bool)] tmp = np.nanargmin(step1 + step2) sInd = sInds[int(np.floor(tmp / float(nStars)))] waitTime = slewTimes[sInd] # Check if exoplanetObsTime would be exceeded mode = list(filter(lambda mode: mode["detectionMode"], allModes))[0] ( maxIntTimeOBendTime, maxIntTimeExoplanetObsTime, maxIntTimeMissionLife, ) = TK.get_ObsDetectionMaxIntTime(Obs, mode) maxIntTime = min( maxIntTimeOBendTime, maxIntTimeExoplanetObsTime, maxIntTimeMissionLife ) # Maximum intTime allowed intTimes2 = self.calc_targ_intTime( np.array([sInd]), TK.currentTimeAbs.copy(), mode ) if ( intTimes2 > maxIntTime ): # check if max allowed integration time would be exceeded self.vprint("max allowed integration time would be exceeded") sInd = None waitTime = 1.0 * u.d return sInd, waitTime
[docs] def revisitFilter(self, sInds, tmpCurrentTimeNorm): """Helper method for Overloading Revisit Filtering Args: sInds - indices of stars still in observation list tmpCurrentTimeNorm (MJD) - the simulation time after overhead was added in MJD form Returns: sInds - indices of stars still in observation list """ tovisit = np.zeros( self.TargetList.nStars, dtype=bool ) # tovisit is a boolean array containing the if len(sInds) > 0: # so long as there is at least 1 star left in sInds tovisit[sInds] = (self.starVisits[sInds] == min(self.starVisits[sInds])) & ( self.starVisits[sInds] < self.nVisitsMax ) # Checks that no star has exceeded the number of revisits if ( self.starRevisit.size != 0 ): # There is at least one revisit planned in starRevisit dt_rev = ( self.starRevisit[:, 1] * u.day - tmpCurrentTimeNorm ) # absolute temporal spacing between revisit and now. ind_rev2 = [ int(x) for x in self.starRevisit[dt_rev < 0 * u.d, 0] if (x in sInds) ] tovisit[ind_rev2] = self.starVisits[ind_rev2] < self.nVisitsMax sInds = np.where(tovisit)[0] return sInds
[docs] def scheduleRevisit(self, sInd, smin, det, pInds): """A Helper Method for scheduling revisits after observation detection Args: sInd - sInd of the star just detected smin - minimum separation of the planet to star of planet just detected det - pInds - Indices of planets around target star Return: updates self.starRevisit attribute """ TK = self.TimeKeeping TL = self.TargetList SU = self.SimulatedUniverse # in both cases (detection or false alarm), schedule a revisit # based on minimum separation Ms = TL.MsTrue[sInd] if ( smin is not None and smin is not np.nan ): # smin is None if no planet was detected sp = smin if np.any(det): pInd_smin = pInds[det][np.argmin(SU.s[pInds[det]])] Mp = SU.Mp[pInd_smin] else: Mp = SU.Mp.mean() mu = const.G * (Mp + Ms) T = 2.0 * np.pi * np.sqrt(sp**3 / mu) t_rev = TK.currentTimeNorm + T / 2.0 # otherwise, revisit based on average of population semi-major axis and mass else: sp = SU.s.mean() Mp = SU.Mp.mean() mu = const.G * (Mp + Ms) T = 2.0 * np.pi * np.sqrt(sp**3 / mu) t_rev = TK.currentTimeNorm + 0.75 * T t_rev = TK.currentTimeNorm.copy() + self.revisit_wait # finally, populate the revisit list (NOTE: sInd becomes a float) revisit = np.array([sInd, t_rev.to("day").value]) if self.starRevisit.size == 0: # If starRevisit has nothing in it self.starRevisit = np.array([revisit]) # initialize starRevisit else: revInd = np.where(self.starRevisit[:, 0] == sInd)[ 0 ] # indices of the first column of the starRevisit list containing sInd if revInd.size == 0: self.starRevisit = np.vstack((self.starRevisit, revisit)) else: self.starRevisit[revInd, 1] = revisit[1] # over