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cosmetic: fix typos in comments

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This commit is contained in:
Mark Whitehorn
2015-08-02 16:07:32 +02:00
committed by Lorenz Meier
parent e443a3f3be
commit c0d2b22d00
1 changed files with 3 additions and 3 deletions
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src/modules/fw_pos_control_l1/mtecs/mTecs.cpp
+3 -3
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@@ -204,7 +204,7 @@ int mTecs::updateFlightPathAngleAcceleration(float flightPathAngle, float flight
mode = tecs_status_s::TECS_MODE_UNDERSPEED;
}
/* Set special ouput limiters if we are not in TECS_MODE_NORMAL */
/* Set special output limiters if we are not in TECS_MODE_NORMAL */
BlockOutputLimiter *outputLimiterThrottle = &_controlTotalEnergy.getOutputLimiter();
BlockOutputLimiter *outputLimiterPitch = &_controlEnergyDistribution.getOutputLimiter();
if (mode == tecs_status_s::TECS_MODE_TAKEOFF) {
@@ -221,7 +221,7 @@ int mTecs::updateFlightPathAngleAcceleration(float flightPathAngle, float flight
outputLimiterPitch = &_BlockOutputLimiterUnderspeedPitch;
}
/* Apply overrride given by the limitOverride argument (this is used for limits which are not given by
/* Apply override given by the limitOverride argument (this is used for limits which are not given by
* parameters such as pitch limits with takeoff waypoints or throttle limits when the launchdetector
* is running) */
limitOverride.applyOverride(*outputLimiterThrottle, *outputLimiterPitch);
@@ -253,7 +253,7 @@ int mTecs::updateFlightPathAngleAcceleration(float flightPathAngle, float flight
(double)accelerationLongitudinalSp, (double)airspeedDerivative);
}
/* publish status messge */
/* publish status message */
_status.update();
/* clean up */