Module/AOA adc - Revision history

Coppolam: Fixed a couple more typos

2017-11-28T09:28:11Z

Fixed a couple more typos

← Older revision		Revision as of 03:28, 28 November 2017
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	== Introduction ==		== Introduction ==

	AOA_adc is a simple module that ~~is be~~ written to test the flight behaviour with a Angle Of Attack sensor.		AOA_adc is a simple module that has been written to test the flight behaviour with a Angle Of Attack sensor.

	It reads the value of an defined ADC port and converts it to ~~and~~ angle.		It reads the value of an defined ADC port and converts it to an angle.

	=== Implementation option A ===		=== Implementation option A ===

Coppolam: Fixed typo

2017-11-28T09:27:11Z

Fixed typo

← Older revision		Revision as of 03:27, 28 November 2017
Line 3:		Line 3:
	== Introduction ==		== Introduction ==

	AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of ~~Attacke~~ sensor.		AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of Attack sensor.

	It reads the value of an defined ADC port and converts it to and angle.		It reads the value of an defined ADC port and converts it to and angle.

Ewoud: /* Hardware */

2013-11-22T13:21:51Z

Hardware

← Older revision		Revision as of 07:21, 22 November 2013
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	Angle of Attack ADC Sensor		Angle of Attack ADC Sensor
	*'''US DIGITAL MA3-A10-236-N'''		*'''US DIGITAL MA3-A10-236-N'''
			If you are using the analog version of this sensor, be sure to connect it to a 5V tolerant ADC on you autopilot. For instance ADC2 on Lisa/M is not 5V tolerant, so a voltage divider is needed to scale the signal down to 3.3V.
	ModuleXML		ModuleXML
	*AOA_adc.xml		*AOA_adc.xml

Openuas at 16:25, 21 November 2013

2013-11-21T16:25:45Z

← Older revision		Revision as of 10:25, 21 November 2013
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	<categorytree style="float:right; clear:right; margin-left:1ex; border: 1px solid gray; padding: 0.7ex;" mode=pages>Modules</categorytree>		<categorytree style="float:right; clear:right; margin-left:1ex; border: 1px solid gray; padding: 0.7ex;" mode=pages>Modules</categorytree>

			== Introduction ==

	AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of Attacke sensor.		AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of Attacke sensor.

	It ~~only~~ reads the value of an defined ADC port and converts it to ~~radiant~~.		It reads the value of an defined ADC port and converts it to and angle.

			=== Implementation option A ===

	A mode variable named h_ctl_pitch_mode in the stabilization_attitude.c enables to switch between estimator_theta (IMU) and estimator_AOA to control the elevator.		A mode variable named h_ctl_pitch_mode in the stabilization_attitude.c enables to switch between estimator_theta (IMU) and estimator_AOA to control the elevator.

	~~Be aware~~: ~~This module is in construction. Feel free to upgrade it.~~		=== Measurements ===

			{TODO: description}

			== Hardware ==

	~~== Module Infos ==~~		{TODO: image}

	Angle of Attack ADC Sensor		Angle of Attack ADC Sensor

Flixr: syntaxhighlight and modules category tree

2012-03-04T23:41:58Z

syntaxhighlight and modules category tree

← Older revision		Revision as of 17:41, 4 March 2012
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			<categorytree style="float:right; clear:right; margin-left:1ex; border: 1px solid gray; padding: 0.7ex;" mode=pages>Modules</categorytree>
	AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of Attacke sensor.		AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of Attacke sensor.

Line 21:		Line 22:

	* (1) '''Insert''' the software module in the airframe:		* (1) '''Insert''' the software module in the airframe:
	<modules>		<source lang="xml">
	<load name="AOA_adc.xml">		<modules>
	<configure name="ADC_AOA" value="ADC_6"/>		<load name="AOA_adc.xml">
	<define name="AOA_OFFSET" value="-0.135000005364"/>		<configure name="ADC_AOA" value="ADC_6"/>
	<define name="AOA_FILTER" value="0.875999987125"/>		<define name="AOA_OFFSET" value="-0.135000005364"/>
	<define name="USE_AOA"/>		<define name="AOA_FILTER" value="0.875999987125"/>
	</load>		<define name="USE_AOA"/>
	</modules>		</load>
			</modules>
			</source>
	* Legend:		* Legend:
	**The ACS_AOA defines on whitch port the US Digital Sensor is connected to.		**The ACS_AOA defines on whitch port the US Digital Sensor is connected to.
Line 38:		Line 41:
	* (3) Now you can turn on the pitch stabilization by setting the '''PITCH_Mode''' to 1		* (3) Now you can turn on the pitch stabilization by setting the '''PITCH_Mode''' to 1
	** PITCH_Mode = 0 --> estimator_thata from IMU (default)		** PITCH_Mode = 0 --> estimator_thata from IMU (default)

			[[Category:Modules]]

Flixr: is already in the master branch

2011-11-03T14:36:38Z

is already in the master branch

← Older revision		Revision as of 08:36, 3 November 2011
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	== Airframe Adjustments ==		== Airframe Adjustments ==
	~~The code is downloadable in the dev branch at the moment:~~
	~~[https://github.com/paparazzi/paparazzi/tree/dev https://github.com/paparazzi/paparazzi/tree/dev]~~

	* (1) '''Insert''' the software module in the airframe:		* (1) '''Insert''' the software module in the airframe:

Flixr: AOA adc moved to Module/AOA adc: moved to Module subdir

2011-11-03T14:35:07Z

AOA adc moved to Module/AOA adc: moved to Module subdir

← Older revision	Revision as of 08:35, 3 November 2011
(No difference)

Bruzzlee: /* Airframe Adjustments */

2011-07-19T22:13:48Z

Airframe Adjustments

← Older revision		Revision as of 16:13, 19 July 2011
Line 19:		Line 19:

	== Airframe Adjustments ==		== Airframe Adjustments ==
			The code is downloadable in the dev branch at the moment:
			[https://github.com/paparazzi/paparazzi/tree/dev https://github.com/paparazzi/paparazzi/tree/dev]

	* (1) '''Insert''' the software module in the airframe:		* (1) '''Insert''' the software module in the airframe:
	<modules>		<modules>

Bruzzlee at 22:08, 19 July 2011

2011-07-19T22:08:22Z

New page

AOA_adc is a simple module that is be written to test the flight behaviour with a Angle Of Attacke sensor.

It only reads the value of an defined ADC port and converts it to radiant.
A mode variable named h_ctl_pitch_mode in the stabilization_attitude.c enables to switch between estimator_theta (IMU) and estimator_AOA to control the elevator.

Be aware: This module is in construction. Feel free to upgrade it.

== Module Infos ==

Angle of Attack ADC Sensor
*'''US DIGITAL MA3-A10-236-N'''
ModuleXML
*AOA_adc.xml
Code- and headerfile
*sw/airborne/modules/sensors
Settings file
*AOA_adc.xml

== Airframe Adjustments ==
* (1) '''Insert''' the software module in the airframe:
<modules>
<load name="AOA_adc.xml">
<configure name="ADC_AOA" value="ADC_6"/>
<define name="AOA_OFFSET" value="-0.135000005364"/>
<define name="AOA_FILTER" value="0.875999987125"/>
<define name="USE_AOA"/>
</load>
</modules>
* Legend:
**The ACS_AOA defines on whitch port the US Digital Sensor is connected to.
**The AOA_OFFSET is needed to adjust the Zero rad mark in the normal flightposition. It can be changed with the AOA_adc.xml settings loaded.
**The AOA_FILTER describes the PT1 filter value of the angle. 0 = no filter
**Define USE_AOA to make the module work.

* (2) '''Load''' the settings XML in the GCS: AOA_adc.xml
* (3) Now you can turn on the pitch stabilization by setting the '''PITCH_Mode''' to 1
** PITCH_Mode = 0 --> estimator_thata from IMU (default)