ardupilot/Tools/LogAnalyzer/tests/TestPitchRollCoupling.py

from LogAnalyzer import Test,TestResult
import DataflashLog

import collections


class TestPitchRollCoupling(Test):
    '''test for divergence between input and output pitch/roll, i.e. mechanical failure or bad PID tuning'''
    # TODO: currently we're only checking for roll/pitch outside of max lean angle, will come back later to analyze roll/pitch in versus out values

    def __init__(self):
        Test.__init__(self)
        self.name = "Pitch/Roll"
        self.enable = True   # TEMP

    def run(self, logdata, verbose):
        self.result = TestResult()
        self.result.status = TestResult.StatusType.GOOD

        if logdata.vehicleType != VehicleType.Copter:
            self.result.status = TestResult.StatusType.NA
            return

        if not "ATT" in logdata.channels:
            self.result.status = TestResult.StatusType.UNKNOWN
            self.result.statusMessage = "No ATT log data"
            return

        # figure out where each mode begins and ends, so we can treat auto and manual modes differently and ignore acro/tune modes
        autoModes   = ["RTL","AUTO","LAND","LOITER","GUIDED","CIRCLE","OF_LOITER","HYBRID"]     # use NTUN DRol+DPit
        manualModes = ["STABILIZE","DRIFT","ALTHOLD","ALT_HOLD","POSHOLD"]                      # use CTUN RollIn/DesRoll + PitchIn/DesPitch
        ignoreModes = ["ACRO","SPORT","FLIP","AUTOTUNE",""]                            # ignore data from these modes
        autoSegments   = []  # list of (startLine,endLine) pairs
        manualSegments = []  # list of (startLine,endLine) pairs
        orderedModes = collections.OrderedDict(sorted(logdata.modeChanges.items(), key=lambda t: t[0]))
        isAuto = False # we always start in a manual control mode
        prevLine = 0
        mode = ""
        for line,modepair in orderedModes.iteritems():
            mode = modepair[0].upper()
            if prevLine == 0:
                prevLine = line
            if mode in autoModes:
                if not isAuto:
                    manualSegments.append((prevLine,line-1))
                    prevLine = line
                isAuto = True
            elif mode in manualModes:
                if isAuto:
                    autoSegments.append((prevLine,line-1))
                    prevLine = line
                isAuto = False
            elif mode in ignoreModes:
                if isAuto:
                    autoSegments.append((prevLine,line-1))
                else:
                    manualSegments.append((prevLine,line-1))
                prevLine = 0
            else:
                raise Exception("Unknown mode in TestPitchRollCoupling: %s" % mode)
        # and handle the last segment, which doesn't have an ending
        if mode in autoModes:
            autoSegments.append((prevLine,logdata.lineCount))
        elif mode in manualModes:
            manualSegments.append((prevLine,logdata.lineCount))

        # figure out max lean angle, the ANGLE_MAX param was added in AC3.1
        maxLeanAngle = 45.0
        if "ANGLE_MAX" in logdata.parameters:
            maxLeanAngle = logdata.parameters["ANGLE_MAX"] / 100.0
        maxLeanAngleBuffer = 10 # allow a buffer margin

        # ignore anything below this altitude, to discard any data while not flying
        minAltThreshold = 2.0

        # look through manual+auto flight segments
        # TODO: filter to ignore single points outside range?
        (maxRoll, maxRollLine)   = (0.0, 0)
        (maxPitch, maxPitchLine) = (0.0, 0)
        for (startLine,endLine) in manualSegments+autoSegments:
            # quick up-front test, only fallover into more complex line-by-line check if max()>threshold
            rollSeg  = logdata.channels["ATT"]["Roll"].getSegment(startLine,endLine)
            pitchSeg = logdata.channels["ATT"]["Pitch"].getSegment(startLine,endLine)
            if not rollSeg.dictData and not pitchSeg.dictData:
                continue
            # check max roll+pitch for any time where relative altitude is above minAltThreshold
            roll  = max(abs(rollSeg.min()),  abs(rollSeg.max()))
            pitch = max(abs(pitchSeg.min()), abs(pitchSeg.max()))
            if (roll>(maxLeanAngle+maxLeanAngleBuffer) and abs(roll)>abs(maxRoll)) or (pitch>(maxLeanAngle+maxLeanAngleBuffer) and abs(pitch)>abs(maxPitch)):
                lit = DataflashLog.LogIterator(logdata, startLine)
                assert(lit.currentLine == startLine)
                while lit.currentLine <= endLine:
                    relativeAlt = lit["CTUN"]["BarAlt"]
                    if relativeAlt > minAltThreshold:
                        roll  = lit["ATT"]["Roll"]
                        pitch = lit["ATT"]["Pitch"]
                        if abs(roll)>(maxLeanAngle+maxLeanAngleBuffer) and abs(roll)>abs(maxRoll):
                            maxRoll = roll
                            maxRollLine = lit.currentLine
                        if abs(pitch)>(maxLeanAngle+maxLeanAngleBuffer) and abs(pitch)>abs(maxPitch):
                            maxPitch = pitch
                            maxPitchLine = lit.currentLine
                    next(lit)
        # check for breaking max lean angles
        if maxRoll and abs(maxRoll)>abs(maxPitch):
            self.result.status = TestResult.StatusType.FAIL
            self.result.statusMessage = "Roll (%.2f, line %d) > maximum lean angle (%.2f)" % (maxRoll, maxRollLine, maxLeanAngle)
            return
        if maxPitch:
            self.result.status = TestResult.StatusType.FAIL
            self.result.statusMessage = "Pitch (%.2f, line %d) > maximum lean angle (%.2f)" % (maxPitch, maxPitchLine, maxLeanAngle)
            return



        # TODO: use numpy/scipy to check Roll+RollIn curves for fitness (ignore where we're not airborne)
        # ...