View source for LinAM V4

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|<categorytree style="float:right; clear:right; margin-left:1ex; border: 1px solid gray; padding: 0.7ex;" mode=pages>Autopilots</categorytree>
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[[Image:LinAM V4 BOX1.jpeg|350px|LinAM V4 BOX1]]
[[Image:LinAM V4 BOX2.png|400px|LinAM V4 BOX2]]
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= <font color="red">LinAM V4</font> =
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== Overview ==

LinAM V4 is based on the 64 pins STM32F405RGT6 Cortex M4 168MHz processor featuring a Floating point unit (FPU), up to 192k of RAM and 1024k of FLASH. 
* STM32 microcontroller datasheet with 1024kB flash and up to 192kB RAM 
* 9 DOF integrated IMU based: '''ADXRS620BBGZ''' Gyro sensor and  '''MXR9150MZ''' Accelerometer with 16 bit ADC ,'''HMC5983''' magnet field sensor. 
* high precision barometer/altimeter '''MS5611-01BA03'''(I2C). 
* Onboard U-Blox GPS '''MAX-M8Q'''.
* Onboard differential pressure sensor '''MPXV5004DP''' (for airspeed) with 16 bit ADC 
* 2 x 3.3V TTL UART (5V tolerant)
* 1 x USB : DFU mode (download) or USB storage (direct access to MicroSD card) 
* 8 x Servo PWM outputs
* 1 x R/C receiver PPM frame input
* 1 x R/C receiver serial input with inverter (Futaba S.BUS, Spektrum, etc.)
* 1 x [http://en.wikipedia.org/wiki/I2c I<sup>2</sup>C] bus
* 1 x CAN bus
* SWD programming/debugging interface.
* 4 x Auxiliary I/O (General Purpose and/or ADC and/or servo PWM).
* 2 x isolated IO for camera control (POWER and SHUTTER).
* Up to 35V (8S LiPo) input power control unit
* Up to 2.5A load current on 5V line
* 1 x 5v/500mA power switch
* 4 x status LEDs
* 20 grams
* 65mm x 45mm 
* 4 layers PCB design
* the box is 89mm x 51mm x 25mm

So, except for a Modem unit with the '''LinAM''' you have all necessary sensors for full features all in one Rotorcraft or Fixedwing solution.

== Hardware Revision History ==
{|border="1"  cellspacing="0" style="text-align:center" cellpadding="6"
!''Version #''!!''Release Date''!!''Release Notes''
|-
|v1.00||07/2014||Initial release of LinAM
|-
|v2.00||11/2014|| LinAM V2
|-
|v3.00||02/2015|| LinAM V3
|-
|v4.00||07/2015|| LinAM V4
|}

== Detailed Features ==

=== 9 DOF IMU ===
* '''ADXRS620BBGZ''' Gyro sensor : quality Gyroscope sensor from Analog Device, it brings one of the best motion sensing performances and vibration immunities in it's class. It ensures much better flight stability and higher immunity to vibration noisy aircrafts.

* '''MXR9150MZ''' Accelerometer: quality acceleration sensor from Memsic sensing solutions, it brings one of the best motion sensing performances and vibration immunities in it's class. It ensures much better flight stability and higher immunity to vibration noisy aircrafts.

* '''HMC5983''' magnet field sensor: Replace HMC5883L temperature compensation triaxial compass.

=== USB Modes ===

* usb plugged before autopilot is powered : enter DFU mode to be flashed

=== SWD: Serial Wire Debug ===
permits flash and source level debugging via swd part of cheap discovery card, or via more capable, fastest, more expensive probe like black magic probe

=== R/C Serial ===

In addition to the classic PPM input, that mostly require receiver modification, one pin of the R/C connector is routed to the MCU UART5 receive input through a '''controlled inverter'''.<br>
This new feature allow '''direct connection''' (3 pin) of several brand off-the-shelf receivers '''without hardware modification''' or external encoder board.
* '''RX5_POL(PA8) = 0''' => R/C serial (Rx5) is '''non-inverted''' : allow use standard polarity serial receivers (Spektrum, FlyElectric...)
* '''RX5_POL(PA8) = 1''' => R/C serial (Rx5) is '''inverted''' : allow use of S.BUS protocol compatible receivers (Futaba, FrSky,...)
(see [[RC_Receivers_and_Radios | R/C Receivers and Radios page]] for serial compatible receiver)

=== Power Switch ===

'''5V''' power output pin on '''AUX connector''' ("5Vaux",#2) '''can be switched ON and OFF''' on demand using APSW (MCU GPIO output PB12).
* APSW(PA15) = 0 => 5V Aux OFF
* APSW(PA15) = 1 => 5V Aux ON (default)
The internal switch TPS2051B is designed to withstand 500mA continuous current and is '''short-circuit and thermally protected'''.<br>
(see [http://www.ti.com/product/tps2051b TPS2051B] datasheet for recommended operation conditions)

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== Pinout ==

Pins Name and Type are specified with respect to the Autopilot Board :[[Media:LinAM_V4_Pinout.pdf|LinAM_V4_Pinout.pdf]]

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[[Image:LinAM_V4_PINOUT.jpeg|900px]]
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{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''POWER IN'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
|-
|B||VBAT||PWR||V_BATT POWER INPUT
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|M||CUR_MEAS||IO||General Purpose I/O(PC0) or ADC_3 Input for current.
|-
|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''AUX'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||5VAUX||PWR||5V from autopilot through [[#Power Switch | Power Switch]]
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|M||RESET||IN||MCU Reset
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''SERVO1/2/3/4/5/6/7/8'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||SRVx||OUT||Servo signal (PWM)
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|M||SERVO_V||PWR||Servo Bus Voltage Rail
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''SBUS/Satellite'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||RX5||IN||UART2 Serial Input (5V Tolerant) through [[#R/C Serial|controlled inverter]]
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|M||+5VDC||PWR||5V Rail from autopilot 
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''PPM'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
|-
|B||RX5||IN||PPM Stream from R/C Receiver or PPM Encoder Board (5V tolerant) 
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|M||+5VDC||PWR||5V Rail from autopilot 
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''ADC/IO'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||ADC2||IO||General Purpose I/O(also spektrum bind pin,PC3) or ADC_2 Input 
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|M||+5VDC||PWR||5V Rail from autopilot 
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''LOG'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||TX3||OUT||USART3 Serial Output (3.3V level)
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|M||+5VDC||PWR||5V Rail from autopilot 
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''TELEM'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||TX3||OUT||USART3 Serial Output (3.3V level)
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|M||RX3||IN||USART3 Serial Input (3.3V level,Pullup(4.7K) to 3.3V)(5V tolerant)
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''SWD'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||SWDCLK||IN||Serial Wire Clock (3.3V level) 
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|M||SWDIO||IO||Serial Wire Data Input/Output (3.3V level) 
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|T||GND||PWR||common ground
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''CAMERA'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||SW||OUT||Connect to camera ON/OFF (PB5,control a PhotoMOS relay)
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|M||SHUT||OUT||Connect to camera shutter (PB4,control a PhotoMOS relay)
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|T||COM||PWR||Connect to camera ground (PhotoMOS relay common)
|}


{|border="1"  cellspacing="0" style="text-align:center" cellpadding="2%" width="70%"
|+'''CAN/I2C'''
!width="7%"|''Pin Pos''!!width="10%"|''Name''!!width="10%"|''Type''!!''Description''
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|B||CANH||IO||CANL (3.3V level) 
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|M||CANL||IO||CANL (3.3V level)
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|T||GND||PWR||common ground
|}

== Pictures ==
<gallery>
Image:LinAM_V4_3D_view_top.jpeg|LinAM V4 3D top view
Image:LinAM_V4_3D_view_bottom.jpeg|LinAM V4 3D bottom view
Image:LinAM_V4_IMU_Vertical_Board.jpeg|LinAM V4 IMU Vertical Board 
Image:LinAM_V4_GPS_AND_AIRSPEED_connector.png|LinAM V4 GPS AND AIRSPEED CONNECTOR
Image:LinAM_V4_PIN.jpeg|LinAM V4 PIN CONNECTOR
Image:LinAM_IMU_V3.jpeg|LinAM V3 IMU BOARD
</gallery>

= Examples of Airborne Equipment Electrical Connections =
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= Programming =

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LinAM autopilot can reprogrammed in two different ways:

* using the MCU native (embedded in rom) DFU USB bootloader over the on-board USB header (so pre-loading an "external" bootloader is useless)
** required hardware : usb cable with usb-mini connector
** required software : dfu_util tool (present in ubuntu repository)
* using the SWD (Serial Wire Debug) connector
** required hardware : usb cable with usb-mini connector, molex to 2.54mm pitch pin cable, swd part of a cheap stm32 evaluation board (any discovery board, start @ 8$)
** required software : st_flash and st_util, have to be compiled from source (https://github.com/texane/stlink)

= Mechanical Dimensions =
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= Schematics =

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= Source code =

Available in latest git master branch

[[Category:Autopilots]]