9. System integration#

9.1. Supported sensors#

IMU

  • Applanix POSAV

  • Applanix AP+

  • all GNSS sending NMEA

  • iXBlue AIRINS / ATLANS

Imaging sensors

  • ITRES

  • Nasa CWIS-II DCS

  • Phase One

  • Simplex

  • UltraCam

LiDAR

  • Riegl

Integrated systems

Sensor mount platforms

  • SOMAG Version 1

  • SOMAG Version 2

  • Aerostab3

  • SteadyTrack

9.2. Setting up a list of SensorHandler integrated sensors#

This chapter is intended for the system integrator only.

9.2.1. The SensorHandler sensor list#

Each button on the left of the SensorHandler panel represents a device being used. Right click on a button to add or remove a device from the list of devices.

../_images/NG_sensor_handler_list.png


ico1 SensorHandler will communicate with Applanix to receive position information and to control the SOMAG platform and, optionally, to take an image.

ico2 SensorHandler will communicate to RiAcquire to start and stop scanning

ico3 In the settings the following information is stored:
  • location of the log files

  • location of the settings files


ico4 Definition of COM ports (not needed in Riegl configuration)

ico5 Definition of Ethernet ports used

9.2.2. SensorHandler Ethernet settings#

In the Ethernet settings dialog, set the IP address and port of each of the devices:

../_images/NG_ethernet.png

9.3. Setting up a PhaseOne camera#

By default, PhaseOne and iXCapture both run on the same computer (usually on an iXController). The operator thus can see the images taken (with iXCapture) while also seeing the navigation window of the flight. This default installation implicates that SensorHandler runs on the same machine.

Some special installations are required to run iXCapture on a different machine than that of the navigation program. In this case, NAVIGATOR and SensorHandler run on one machine and iXCapture on another.

9.4. Setting up a universal camera#

By using an external trigger cable it is possible to control any kind of camera.

Requirements:

  • external trigger cable (camera specific)

  • optional: hot shoe adapter (incl. cable)

  • the cables are connected to the flight computer via COM port

9.5. Setting up Riegl RiAcquire#


The sketch below illustrates two methods for triggering the camera to capture an image.

../_images/NG_CAMtrigger_paths.png

In the standard method (A), the image capture settings are configured in the SensorHandler RiAcquire menu. These settings are then transferred to RiAcquire, which communicates directly with the camera to trigger the image.

In the alternative method (B), the settings are configured in the SensorHandler POSAV menu. These settings are passed to the IMU, which in turn communicates with the camera to trigger the image.

9.6. Setting up Applanix AP+#

Important

Configure the GSOF as described in the chapter Setting up Applanix in AVX210.

SensorHandler needs two ports to communicate with Applanix AP+:

  • TCP/IP to get navigation data (it is usually defined as port 28001)

  • TCP/IP to get event information (it is usually defined as port 28002)

9.6.1. Definition in web interface of Applanix AP+#

Ports 28001 and 28002 are used. These are the default ports but other port numbers can also be used.

../_images/NG_Applanix_1.png

Definitions for navigation data (port 28001):

../_images/NG_Applanix_2.png

Definitions for event (port 28002):

../_images/NG_Applanix_3.png

9.6.2. Settings in SensorHandler#

Important

Note for conducting Riegl scanners
If the images will be released through the RiAcquire interface, then do NOT enable the Trigger images option:
../_images/NG_Applanix_SH7.png

Enable it in the RiAcquire dialog instead:

../_images/NG_Applanix_SH8.png

9.6.3. Remarks for controlling a gyro mount#

../_images/NG_gyromount1.png
If the system is leveled using a mount, the corresponding option must be set.
The figure shows that the mount is switched to STAB mode 30 seconds before the start of the line.

Important

The mount will only switch to STAB mode (unfreeze) when the aircraft is inside the corridor.


../_images/NG_gyromount2.png

The green box signifies that the mount is in MAN mode (freeze). The aircraft is outside the corridor, so the two buttons (set manually ON, set manually OFF) can be activated.

../_images/NG_gyromount3.png

The green box signifies that the mount is in STAB mode (unfreeze). The aircraft is inside the corridor. Therefore, the two buttons (Set manually ON, set manually OFF) cannot be activated.

../_images/NG_gyromount4.png

A prompt indication of whether the mount is in stabilization mode is provided through the icon displayed in the main window of the NAVIGATOR program, see Status of MNT - SOMAG Mount.

9.7. Setting up Applanix POSAV#

9.7.1. Settings in Applanix POSView program#

The Applanix program POSView controls the IMU settings. Make sure the following settings are made in POSView Ethernet Real-Time Port 2:

../_images/NG_POSView.png

Enable the following groups:

  • 1: Navigation solution

  • 3: Primary GNSS Data

  • 5: Event 1

  • 200: Gimbal Encoder Data

  • 203: Gimbal Yaw Drift Correction Data

  • 222: Reference frame Navigation solution, only if you use direct control of the mount with the special handler for somag mount V2 (by default group 222 is not activated).

    ../_images/NG_somag.png

Store the settings in PosView:

../_images/NG_POSView1.png

9.8. Setting up Applanix in AVX210#

9.8.1. Settings for GSOF in AVX210#

../_images/NG_GSOF4.png

The following GSOF messages need to be transmitted:

../_images/NG_GSOF5.png

The following NMEA message needs to be transmitted:

../_images/NG_GSOF6.png

Hint

Background information: NMEA altitudes are referenced to the EGM96 geoid. Most often, the planned altitudes for the lines of flight are also referenced to the EGM96. GSOF Message 9, however, is referenced to the WGS84 ellipsoid. In most cases, the flight has to be done on EGM96 altitudes. Therefore, NMEA GGA needs to know the difference between EGM96 and WGS84 altitudes.

../_images/NG_GSOF7.png

../_images/NG_GSOF8.png

../_images/NG_GSOF9.png

9.9. Setting up Novatel using NMEA#

The integration into SensorHandler follows the same approach as outlined here for NMEA.

The Novatel Ethernet and port settings may appear as shown in this example (192.168.53.100 and 3005):

../_images/NG_config_NMEA_2.png

9.10. Setting up NMEA#

Any device capable of sending NMEA sentences is compatible with NAVIGATOR. For navigation, only the following sentences are needed:

  • GPGGA

  • GPVTG

9.10.1. Settings up NMEA GPS in SensorHandler#

Hint

Remember to define the port (COM or TCP) through which the device can be reached.

9.10.2. Settings for NMEA in SensorHandler for TCP/IP or UDP#

9.10.3. Settings for NMEA in AVX210#

If NMEA is the protocol, then use the settings shown below:

../_images/NG_NMEA_protocol.png

../_images/NG_NMEA_protocol1.png

9.11. Using the SOMAG mount handler#

9.11.1. The two main configurations#

Important

To control the SOMAG mount this question must be answered: which device controls the mount?
Is it a) the Flight Management system or b) the INSS?
If using POS AV, then a) and b) can both be applied.
If using Novatel, then only a) is possible.
../_images/NG_mount_control.png
../_images/NG_mount_control1.png ../_images/NG_mount_control2.png

1 POS AV or any other INSS sends position data to the FMS. This is usually done by Ethernet but it can also be done by serial communication.

1 POS AV sends position data to the FMS.

The FMS sends freeze / unfreeze to POS AV

2 The FMS is connected to the mount by a serial port. The FMS does the whole control of the mount:

  • Changing to STAB and MAN before and after the line

  • Sending pitch, roll and yaw corrections to the mount

  • Reading the mount angles

2 POS AV is connected to the mount. POS AV fully controls the mount:

  • Changing to STAB and MAN before and after the line

  • Sending pitch, roll and yaw corrections to the mount

  • Reading the mount angles

No mount angles are logged.

The mount angles can be logged on POS AV.

9.11.2. Basic modes of operation#

This handler is used to control all the gyro mounts of the SOMAG AG Jena, running Protocol Version 2.0 .

../_images/NG_basicmode.png

In standard mode, the mount will be set to STAB mode before the line of flight starts and will be set to MAN mode after the line has been finished or when the line is left. The following angles need to be known to drive the mount accurately to the needed position:

  • pitch, roll, heading angles coming from the IMU

  • ground track heading coming from the GPS

  • actual yaw angle of the mount

  • the desired heading angle the mount should to be driven to. This heading angle can either be the heading of the planned line of flight or of the ground track.

For special cases (like testing the mount), the automatic control of the mount can be switched off:

../_images/NG_basicmode.png

After switching off the automatic mode, the mount won’t switch between MAN and STAB mode automatically. This mode is mostly used for testing system components like communication and behavior of the mount.

9.11.3. Pre-flight settings#

../_images/NG_preflight.png
../_images/NG_settings_number1.png
By default, heading corrections are switched ON. This means that the IMU yaw angle will be corrected in accordance with the received IMU angles. SensorHandler requires the actual yaw of the gimbal in order to calculate the amount of correction for accurate yaw positioning of the mount. Here, you set the time intervals in which actual gimbal angles are sent to SensorHandler. Normally, a value of 100 milliseconds is used.

Select the method for heading correction:
  • Heading correction in STAB mode: this is the default. The mount is set to STAB mode at the start of the line and to MAN mode after having left the line.

  • Heading correction in MAN mode: in this mode, the mount’s heading correction is carried out only by SensorHandler. No correction will be performed by the mount. This mode can be useful for ground tracks with short and intense changes in the heading (e.g. flying along a river or road by helicopter).

  • Set drift to Planned Heading: this is the default. TOPOFLIGHT NAVIGATOR sends the line’s heading to SensorHandler. SensorHandler then sends small corrections to the mount to accurately align it with the line’s heading.

  • Set drift to Ground Track: the yaw angle of the mount will be directed towards the ground track.

The following sketch illustrates the distinction between the modes Set Drift to Ground Track (on the left) and Set Drift to Planned Heading (right):

../_images/NG_driftsketch.png
../_images/NG_settings_number2.png

The default position is switched ON. This means that roll and pitch angles coming from the IMU are used to increase the accuracy of the mount’s stabilization process during flight.

../_images/NG_settings_number3.png

In the edit fields, you define how many seconds before the start of the line of flight the mount will go into STAB mode and how many seconds after the end of the line of flight the mount will switch back to MAN mode.

9.11.4. Automatic transition between STAB and MAN mode#

../_images/NG_stabmanmode1.png

../_images/NG_stabmanmode2.png

While on the line of flight the mount is automatically set to STAB mode

../_images/NG_stabmanmode3.png

After having left the line of flight the mount is automatically switched back to MAN mode

9.11.5. Manual transition between STAB and MAN mode#

../_images/NG_stabmanmode4.png

../_images/NG_stabmanbutton1.png

switches back to automatic mode

../_images/NG_stabmanbutton2.png

sets the STAB mode for all axes (roll, pitch, yaw)

../_images/NG_stabmanbutton3.png

STAB mode is switched off and MAN mode is activated

../_images/NG_stabmanbutton4.png
  • When the FMS control is switched OFF the mount can only be manually driven with using the SOMAG app. In this case, no commands from SensorHandler will be received.

  • When the FMS control is switched ON the mount is driven only by SensorHandler. No commands from the SOMAG app will be received.

9.11.6. For system integrators: COM port settings#

The SOMAG mount and SensorHandler communicate through serial communication, requiring accurate configuration of the corresponding COM port settings.

Tip for system Integrators

Important

Read the section below on how to verify the proper functionality of SensorHandler in conjunction with the SOMAG mount!

Often, when integrating a system, you have the mount on the table but do not yet have an IMU available. Switch the mount without a connected IMU to STAB mode. You will notice that the mount moves slightly to the end stops (it does not really stabilize). But you can check if SensorHandler and mount behave correctly.

You can perform this system check by forcing SensorHandler to send the mount gimbal angles back to the mount as simulated IMU values. Then the mount will be stabilized on the table. Do the following:

9.12. Setting up ITRES sensor handling#

9.13. Setting up TOPOFLIGHT universal sensor handling#

Hint

Go to the chapter TOPOFLIGHT universal protocol for a detailed description of the socket usage, the TCP message structure, the states and state switches as well as the usage of the TOPOFLIGHT universal protocol.

../_images/NG_TF_uni_prot.png
../_images/NG_settings_number1.png

As the airplane is aligned to the flight line and passed the defined time, an Acquire dark frame command is sent to the system.

../_images/NG_settings_number2.png

As the airplane passes this time marker, NAVIGATOR will be informed that the airplane approaches the first point. This command is not used right now.

../_images/NG_settings_number3.png

As the airplane passes this time marker, the start logging command will be sent to the system.

../_images/NG_settings_number4.png

As the airplane passes this time marker, an Acquire dark frame command will be sent to the system followed by a stop logging command.

../_images/NG_settings_number5.png

When the airplane leaves the corridor (before it reached the end of the line) and does not enter within the defined time then a stop logging command will be sent to the system.