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ArduPlane supports the use of an airspeed sensor (such as the one shown above), which can help in windy condition, slow flight and autonomous landings. It is not recommended for most new users, however, as it does require additional tuning and adds one more layer of control to set up.
The way it works is that the top tube is “active” (measures air pressure from the pitot tube that is open at the front and has air driven into it by airspeed) and the bottom one is “static” (measures ambient air pressure from tube with intakes on the side).
Connect the active sensor port using silicon tube to the straight tube exiting from the rear of the pitot tube. The angled tube is the static part connecting to the static port of the sensor (the port on the sensor closest to the PCB breakout board)
After you install an airspeed sensor don’t forget to calibrate it!
Here’s how to hook it up:
Plug it into the pins on the “A0″ port, as shown:
A digital airspeed sensor is available for Pixhawk from store.3dr.com. Connect the airspeed sensor to Pixhawk’s I2C port (or I2C splitter module). Using the rubber tubing, connect the longer extension on the pitot tube to the cone that protrudes from the top of the airspeed sensor board (off the off-white, square section protruding off the top of the board), and connect the shorter extension on the pitot tube to the cone protruding from the base of the board.
To enable the digital airspeed sensor, connect Pixhawk to Mission Planner (or APM Planner for OS X), and select the Advanced Parameter Listunder the Configuration tab. Locate the ARSPD_PIN parameter and set to 65. Select Write Params to apply. Ensure that you have also enabled the airspeed sensor in the setup section (Mission Planner -> Hardware -> Optional Hardware -> Airspeed).
You need to enable the airspeed sensor in (Mission Planner -> Hardware -> Optional Hardware -> Airspeed). You can test that it is working in the CLI by using the “airspeed” command in the “test” menu.
Note: Oscillation between zero and small values (2-3) is normal. The airspeed varies with the square root of the pressure, so for differential pressures near zero it varies quite a bit with very small pressure changes, while at flying speeds it takes much greater pressure changes to produce a similar change in speed. If you see mostly 0, 1, 2, with an occasional bounce to 3 or 4, consider it normal. You will not see that sort of variability at flying speeds. As a check, you can take the fleshy part of your fingertip and press it against the pitot tube to raise the airspeed reading up to say 15 m/s. It is easy to see that holding a significant constant differential pressure like this the reading does not bounce around (if you keep constant pressure).
Once you have the airspeed sensor connected, you can use it to control aircraft speed in auto modes. Change the “Cruise” setting in the Tuning screen of either APM Planner (shown) or Mission Planner:
When you place the airspeed sensor in your aircraft, use this pitot tube set
. The kit comes with a single tube to measure both static and total pressure. In the case of the !EasyStar, you’ll need to push it through the foam in the cockpit so it points straight into the airstream. Make sure the holes in the side of the tube are not covered. They should be at least 1 centimeter out past the nose. First connect the two tubes coming out the back to the airspeed sensor. The tube coming straight out the back should go into the top port and the tube exiting at an angle should connect to the bottom port on the airspeed sensor. Drill or cut a small hole in the foam and push it through to the front.
If you are using APM in an aircraft with the propeller in the nose, the pitot tube must be mounted out on one wing, at least a foot from the fuselage to be outside the prop flow.
You can check the airspeed reading with Mission Planner or another ground station. Just blow on the pitot tube and observe the response. In still air oscillation between zero and small values (2-3) is normal. The airspeed varies with the square root of the pressure, so for differential pressures near zero it varies quite a bit with very small pressure changes, while at flying speeds it takes much greater pressure changes to produce a similar change in speed. If you see mostly 0, 1, 2, with an occasional bounce to 3 or 4, consider it normal. You will not see that sort of variability at flying speeds.
You can also check it with the ArduPlane CLI in the Mission Planner’s terminal screen. Just go into CLI/test menu and type “airspeed”. Detailshere
The airspeed sensor reading is automatically zeroed by the APM during initialisation, so it is good practice during windy conditions to place a loose fitting cover over the pitot tube that shields the front hole and the four small side holes from the wind. This cover should be fitted prior to power on and removed before flight. If you forget to do this, you can always place the cover and repeat the airspeed auto-zero using the Mission Planners PREFLIGHT_CALIBRATE => Do Action.
The airspeed reading scale factor is adjusted using the ARSPD_RATIO parameter. APM:Plane has an automatic calibration function that will adjust the value of ARSPD_RATIO automatically provided the plane is flown with frequent direction changes. A normal model flying field circuit pattern or loiter will achieve the required direction changes, cross-country flying will not. To enable automatic airspeed sensor calibration, set the value of ARSPD_AUTOCAL to 1.