Http ardupilot org plane

This is a set of frequently asked questions with answers.

Before you can fly your plane you need to arm it. Arming the aircraft before flight has two purposes:. The key thing that arming does is to enable the motor. You will not be able to start the motor ie. Flying EKF without arming checks may cause a crash. This feature in no way removes the need to respect the prop!

Http ardupilot org plane

Plane has a wide range of built in flight modes. Plane can act as a simple flight stabilization system, a sophisticated autopilot, a training system or a flight safety system depending on what flight mode and options you choose. Flight modes are controlled through a radio transmitter switch , via mission commands, or using commands from a ground station GCS or companion computer. All of the flight modes below have optional additional controls that may be used to change the behaviour to suit particular flying needs. After you have read the introductory material below it is highly recommended that you look through the complete set of Plane parameters so you can explore the full range of functionality available. Most altitude controlled modes can optionally maintain altitude with respect to Terrain instead of relative to HOME. See Terrain Following for more information. Any stabilized control mode requires tuning for optimal performance. Tune TECS before using automatic throttle modes extensively. Note Most altitude controlled modes can optionally maintain altitude with respect to Terrain instead of relative to HOME.

If it is 0, then the plane will terminate in any flight mode. This controls the minimum altitude change for a waypoint before a glide slope will be used instead of an immediate altitude change.

Plane is an advanced open-source autopilot firmwware system for conventional planes, flying wings, and VTOL capable QuadPlanes. It offers a wide variety of flight modes from fully manual to fully autonomous. It also benefits from other parts of the ArduPilot ecosystem, including simulators, log analysis tools, and higher level APIs for vehicle control. ArduPilot is already a preferred software platform for numerous commercially available autopilot systems but you can also use it to enhance the abilities of your own DIY planes or convert normal RC only systems into fully featured autonomous aircraft. Please do not be tempted to skip over steps and rush into flight.

This article provides information to help you get started with airframe tuning. It includes an overview of the main steps, tools and concepts. With the default PID settings, Plane will fly the majority of lightweight RC airframes not full size, full speed airframes safely, right out of the box. The most important configuration is Roll and Pitch tuning, as this is essential for responsive and stable flight as well as effective navigation. Plane will fly the majority of lightweight RC airframes right out of the box. We also provide configuration values for many common aircraft that you can use to get your aircraft flying before doing further tuning. After tuning the Roll, Pitch and optionally yaw you should tune the height controller using the TECS tuning guide and the horizontal navigation using the L1 controller tuning guide. Information on how to tune other aspects of Plane are linked from the Tuning landing page. This section will be updated in the future for 4. The column on the left links to the full parameter set.

Http ardupilot org plane

Plane is an advanced open-source autopilot firmwware system for conventional planes, flying wings, and VTOL capable QuadPlanes. It offers a wide variety of flight modes from fully manual to fully autonomous. It also benefits from other parts of the ArduPilot ecosystem, including simulators, log analysis tools, and higher level APIs for vehicle control. ArduPilot is already a preferred software platform for numerous commercially available autopilot systems but you can also use it to enhance the abilities of your own DIY planes or convert normal RC only systems into fully featured autonomous aircraft. Please do not be tempted to skip over steps and rush into flight. This is robotics and aviation combined — both of which are quite complex on their own.

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Spacing the waypoints a little further away would have allowed the approach to have settled by the final approach waypoint, and with the desired final glide slope. The default is 0. Not all of these autopilots have been directly tested by ArduPilot development team members and while firmware is provided by ArduPilot, it does not constitute an endorsement by ArduPilot. The APM2. Analog input pin that fuel level sensor is connected to. Maximum bank angle commanded in modes with stabilized limits. Enables automatic adjustment of airspeed ratio during a calibration flight based on estimation of ground speed and true airspeed. Try sending an arm command with your GCS. This controls the height above the glide slope the plane may be before rebuilding a glide slope. However, the actual result is 9 deg glide path since the switch to AUTO mode and the landing sequence was begun at the point shown at beginning of the yellow path, and the resulting overshoots at the two waypoints result in a steeper glide slope 9 degrees between the final approach waypoint and the touchdown point. See the wiki for each vehicle. Without airspeed sensor, uses synthetic airspeed from wind speed estimate that may both be inaccurate. Remember to turn it back on before you fly. The reason is the new stall prevention code. With a Pixhawk using the 3DR Power brick this should be set to

With ArduPilot AP it is possible to use a fully functional, powerful autonomous flight system on inexpensive, highly integrated autopilot boards, including onboard battery monitoring and an onboard OSD. This guide attempts to provide the necessary instructions to get airborn on a typical ArduPlane setup with autonomous flight fleatures and is intentionally focussing only a small part of what ArduPilot has to offer. For a more in-depth explanation of flight features see the full setup guide.

For Synthetic Current sensor monitors, this is the maximum, full throttle current draw. This is the ratio of static pressure error to dynamic pressure generated by a negative wind relative velocity along the Y body axis. Mode can still be accessed via RC or failsafe. This can be caused by temperature changes. The techniques are:. Note Not all of these autopilots have been directly tested by ArduPilot development team members and while firmware is provided by ArduPilot, it does not constitute an endorsement by ArduPilot. This is the ratio of static pressure error to dynamic pressure generated by a negative wind relative velocity along the Z body axis. The sections below provide information about ArduPilot autopilot hardware options. Before you can fly your plane you need to arm it. Before allowing arming the autopilot checks a set of conditions. This option takes affect on next boot. Keep up with the latest ArduPilot related blogs on ArduPilot. Enables roll limits at low airspeed in roll limiting flight modes. We are looking at ways of detecting partial airspeed sensor failures and hope to add some protection into the code in the future. This is the ratio of static pressure error to dynamic pressure generated by a positive wind relative velocity along the Y body axis.