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| Author | SHA1 | Date | |
|---|---|---|---|
| eb8faa9c10 | |||
| 165c0cefa9 | |||
| 131bbd9f0a | |||
| dd70e5ddb2 | |||
| a65299be26 | |||
| 7174c16628 |
32
main.lua
32
main.lua
@@ -410,11 +410,11 @@ local function populateThrusterValues()
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thruster.power = thruster.thruster.getPower()
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thruster.power = thruster.thruster.getPower()
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elseif thruster.type == "rotator" then
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elseif thruster.type == "rotator" then
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if thruster.transmission ~= nil then
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if thruster.transmission ~= nil then
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local transmissionType = peripheral.getType(thruster.transmission)
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local transmissionType = peripheral.getType(peripheral.wrap(thruster.transmission))
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if transmissionType == "analog_transmission" then
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if transmissionType == "analog_transmission" then
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thruster.power = (thruster.transmission.getSignal())/15
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thruster.power = (peripheral.wrap(thruster.transmission).getSignal())/15
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elseif transmissionType == "Create_RotationSpeedController" then
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elseif transmissionType == "Create_RotationSpeedController" then
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thruster.power = (thruster.transmission.getTargetSpeed())/256
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thruster.power = (peripheral.wrap(thruster.transmission).getTargetSpeed())/256
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end
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end
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else
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else
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print("ERROR: Thruster "..peripheral.getName(thruster.thruster).." has no transmission.")
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print("ERROR: Thruster "..peripheral.getName(thruster.thruster).." has no transmission.")
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@@ -789,7 +789,7 @@ function SetThrusterPower(thruster, power)
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if power > 1.0 then power = 1.0 elseif power < 0.0 then power = 0.0 end
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if power > 1.0 then power = 1.0 elseif power < 0.0 then power = 0.0 end
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if Config.Debug then print("DEBUG: thruster "..thruster.name..": power "..power) end
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--if Config.Debug then print("DEBUG: thruster "..thruster.name..": power "..power) end
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if thruster.type == "rotator" then
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if thruster.type == "rotator" then
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thruster.power = power
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thruster.power = power
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@@ -862,15 +862,15 @@ function CreatePID(kp, ki, kd)
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integral = 0, lastError = 0,
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integral = 0, lastError = 0,
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minOutput = 0.0,
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minOutput = 0.0,
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maxOutput = 64.0,
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maxOutput = 32.0,
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update = function(self, setpoint, pv, dt)
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update = function(self, setpoint, pv, dt)
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if dt <= 0 then return 0.0 end
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local error = setpoint - pv
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local error = setpoint - pv
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local P = self.kp * error
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local P = self.kp * error
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local D = 0
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local D = self.kd * ((error - self.lastError) / dt)
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if dt > 0 then D = self.kd * ((error - self.lastError) / dt) else D = 0 end
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local potential_i = self.integral + (self.ki * error * dt)
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local potential_i = self.integral + (self.ki * error * dt)
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@@ -880,7 +880,7 @@ function CreatePID(kp, ki, kd)
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local clampedOutput = 0
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local clampedOutput = 0
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if self.minOutput <= potential_i and potential_i <= self.maxOutput then
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if raw_output >= self.minOutput and raw_output <= self.maxOutput then
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self.integral = potential_i
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self.integral = potential_i
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clampedOutput = raw_output
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clampedOutput = raw_output
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else
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else
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@@ -889,9 +889,7 @@ function CreatePID(kp, ki, kd)
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self.lastError = error
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self.lastError = error
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local normalizedOutput = (clampedOutput - self.minOutput) / (self.maxOutput - self.minOutput)
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return clampedOutput
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return normalizedOutput
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end
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end
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}
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}
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end
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end
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@@ -900,13 +898,13 @@ end
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PIDs = {
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PIDs = {
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-- angular
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-- angular
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-- attitude PIDs
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-- attitude PIDs
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RollAttitudePID = CreatePID(4.5, 0.01, 0.05),
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RollAttitudePID = CreatePID(3.0, 0.01, 0.05),
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PitchAttitudePID = CreatePID(4.5, 0.01, 0.05),
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PitchAttitudePID = CreatePID(3.0, 0.01, 0.05),
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YawAttitudePID = CreatePID(0.1, 0.01, 0.05),
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YawAttitudePID = CreatePID(0.1, 0.01, 0.05),
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-- rate PIDs
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-- rate PIDs
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RollRatePID = CreatePID(1.2, 0.01, 0.05),
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RollRatePID = CreatePID(0.8, 0.01, 0.05),
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PitchRatePID = CreatePID(1.2, 0.01, 0.05),
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PitchRatePID = CreatePID(0.8, 0.01, 0.05),
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YawRatePID = CreatePID(0.5, 0.01, 0.05),
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YawRatePID = CreatePID(0.5, 0.01, 0.05),
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-- lateral
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-- lateral
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@@ -916,7 +914,7 @@ PIDs = {
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ForeAftPID = CreatePID(0.1, 0.01, 0.05),
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ForeAftPID = CreatePID(0.1, 0.01, 0.05),
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-- rate PIDs
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-- rate PIDs
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VerticalRatePID = CreatePID(1.2, 0.01, 0.05),
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VerticalRatePID = CreatePID(0.8, 0.01, 0.05),
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PortStarRatePID = CreatePID(0.1, 0.01, 0.05),
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PortStarRatePID = CreatePID(0.1, 0.01, 0.05),
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ForeAftRatePID = CreatePID(0.1, 0.01, 0.05)
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ForeAftRatePID = CreatePID(0.1, 0.01, 0.05)
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}
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}
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@@ -997,6 +995,8 @@ function UpdateGlobalThrust()
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SetThrusterPower(thruster, desiredThrust)
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SetThrusterPower(thruster, desiredThrust)
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else
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else
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if Config.Debug then print("DEBUG: Thruster has x_config_equivalent set") end
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local prop1 = throttleOutput + pitchRateOutput + rollRateOutput -- front-left
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local prop1 = throttleOutput + pitchRateOutput + rollRateOutput -- front-left
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local prop2 = throttleOutput + pitchRateOutput - rollRateOutput -- front-right
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local prop2 = throttleOutput + pitchRateOutput - rollRateOutput -- front-right
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local prop3 = throttleOutput - pitchRateOutput - rollRateOutput -- back-right
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local prop3 = throttleOutput - pitchRateOutput - rollRateOutput -- back-right
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