INAV Programming Framework (IPF)

INAV Programming Framework (IPF) is a mechanism that allows you to to create custom functionality in INAV. You can choose for certain actions to be done based on custom conditions you select.

Logic conditions can be based on things such as RC channel values, switches, altitude, distance, timers, etc. The conditions you create can also make use of other conditions you've entered previously. The results can be used in:

• Servo mixer to activate/deactivate certain servo mix rulers
• To activate/deactivate system overrides

INAV Programming Framework consists of:

• Logic Conditions - each Logic Condition can be understood as a single command, a single line of code. Each logic condition consists of:
  • an operator (action), such as "plus" or "set vtx power"
  • one or two operands (nouns), which the action acts upon. Operands are often numbers, such as a channel value or the distance to home.
  • "activator" condition - optional. This condition is only active when another condition is true
• Global Variables - variables that can store values from and for Logic Conditions and servo mixer
• Programming PID - general purpose, user configurable PID controllers

IPF can be edited using INAV Configurator user interface, or via CLI. To use COnfigurator, click the tab labeled "Programming". The various options shown in Configurator are described below.

Note: IPF uses integer math. If your programming line returns a decimal, it will be truncated to an integer. So if your math is 1 / 3 = , IPF will truncate the decimal and return 0.

JavaScript-Based Programming (Alternative)

INAV also supports a JavaScript-based programming interface that provides a more familiar syntax for those comfortable with JavaScript. The JavaScript code is transpiled (converted) into traditional logic conditions, so both methods ultimately use the same underlying system.

See the JavaScript Programming Guide for complete documentation on using JavaScript to program your flight controller.

Benefits of JavaScript programming:

• Modern code editor with IntelliSense autocomplete
• Real-time syntax validation and error messages
• Familiar programming constructs (if statements, functions, variables)
• Automatic conversion to logic conditions

Logic Conditions

CLI

logic <rule> <enabled> <activatorId> <operation> <operand A type> <operand A value> <operand B type> <operand B value> <flags>

• <rule> - ID of Logic Condition rule
• <enabled> - 0 evaluates as disabled, 1 evaluates as enabled
• <activatorId> - the ID of LogicCondition used to activate this Condition. Logic Condition will be evaluated only then Activator evaluates as true. -1 evaluates as true
• <operation> - See Operations paragraph
• <operand A type> - See Operands paragraph
• <operand A value> - See Operands paragraph
• <operand B type> - See Operands paragraph
• <operand B value> - See Operands paragraph
• <flags> - See Flags paragraph

Operations

Operation ID	Name	Notes
0	True	Always evaluates as true
1	Equal (A=B)	Evaluates false if false or 0
2	Greater Than (A>B)	true if Operand A is a higher value than Operand B
3	Lower Than (A<B)	true if Operand A is a lower value than Operand B
4	Low	true if <1333
5	Mid	true if >=1333 and <=1666
6	High	true if >1666
7	AND	true if Operand A and Operand B are the same value or both true
8	OR	true if Operand A and/or OperandB is true
9	XOR	true if Operand A or Operand B is true, but not both
10	NAND	false if Operand A and Operand B are both true
11	NOR	true if Operand A and Operand B are both false
12	NOT	The boolean opposite to Operand A
13	Sticky	Operand A is the activation operator, Operand B is the deactivation operator. After the activation is true, the operator will return true until Operand B is evaluated as true
14	Basic: Add	Add Operand A to Operand B and returns the result
15	Basic: Subtract	Substract Operand B from Operand A and returns the result
16	Basic: Multiply	Multiply Operand A by Operand B and returns the result
17	Basic: Divide	Divide Operand A by Operand B and returns the result. NOTE: If Operand B = 0, the Divide operation will simply return Operand A
18	Set GVAR	Store value from Operand B into the Global Variable addressed by Operand A. Bear in mind, that operand Global Variable means: Value stored in Global Variable of an index! To store in GVAR 1 use Value 1 not Global Variable 1
19	Increase GVAR	Increase the GVAR indexed by Operand A (use Value 1 for Global Variable 1) with value from Operand B
20	Decrease GVAR	Decrease the GVAR indexed by Operand A (use Value 1 for Global Variable 1) with value from Operand B
21	Set IO Port	Set I2C IO Expander pin Operand A to value of Operand B. Operand A accepts values 0-7 and Operand B accepts 0 and 1
22	Override Arming Safety	Allows the craft to arm on any angle even without GPS fix. WARNING: This bypasses all safety checks, even that the throttle is low, so use with caution. If you only want to check for certain conditions, such as arm without GPS fix. You will need to add logic conditions to check the throttle is low.
23	Override Throttle Scale	Override throttle scale to the value defined by operand. Operand type 0 and value 50 means throttle will be scaled by 50%.
24	Swap Roll & Yaw	basically, when activated, yaw stick will control roll and roll stick will control yaw. Required for tail-sitters VTOL during vertical-horizonral transition when body frame changes
25	Set VTx Power Level	Sets VTX power level. Accepted values are 0-3 for SmartAudio and 0-4 for Tramp protocol
26	Invert Roll	Inverts ROLL axis input for PID/PIFF controller
27	Invert Pitch	Inverts PITCH axis input for PID/PIFF controller
28	Invert Yaw	Inverts YAW axis input for PID/PIFF controller
29	Override Throttle	Override throttle value that is fed to the motors by mixer. Operand is scaled in us. 1000 means throttle cut, 1500 means half throttle
30	Set VTx Band	Sets VTX band. Accepted values are 1-5
31	Set VTx Channel	Sets VTX channel. Accepted values are 1-8
32	Set OSD Layout	Sets OSD layout. Accepted values are 0-3
33	Trigonometry: Sine	Computes SIN of Operand A value in degrees. Output is multiplied by Operand B value. If Operand B is 0, result is multiplied by 500
34	Trigonometry: Cosine	Computes COS of Operand A value in degrees. Output is multiplied by Operand B value. If Operand B is 0, result is multiplied by 500
35	Trigonometry: Tangent	Computes TAN of Operand A value in degrees. Output is multiplied by Operand B value. If Operand B is 0, result is multiplied by 500
36	Map Input	Scales Operand A from [0 : Operand B] to [0 : 1000]. Note: input will be constrained and then scaled
37	Map Output	Scales Operand A from [0 : 1000] to [0 : Operand B]. Note: input will be constrained and then scaled
38	Override RC Channel	Overrides channel set by Operand A to value of Operand B. Note operand A should normally be set as a "Value", NOT as "Get RC Channel"
39	Set Heading Target	Sets heading-hold target to Operand A, in centidegrees. Value wraps-around.
40	Modulo	Modulo. Divide Operand A by Operand B and returns the remainder
41	Override Loiter Radius	Sets the loiter radius to Operand A [0 : 100000] in cm. Must be larger than the loiter radius set in the Advanced Tuning.
42	Set Control Profile	Sets the active config profile (PIDFF/Rates/Filters/etc) to Operand A. Operand A must be a valid profile number, currently from 1 to 3. If not, the profile will not change
43	Use Lowest Value	Finds the lowest value of Operand A and Operand B
44	Use Highest Value	Finds the highest value of Operand A and Operand B
45	Flight Axis Angle Override	Sets the target attitude angle for axis. In other words, when active, it enforces Angle mode (Heading Hold for Yaw) on this axis (Angle mode does not have to be active). Operand A defines the axis: 0 - Roll, 1 - Pitch, 2 - Yaw. Operand B defines the angle in degrees
46	Flight Axis Rate Override	Sets the target rate (rotation speed) for axis. Operand A defines the axis: 0 - Roll, 1 - Pitch, 2 - Yaw. Operand B defines the rate in degrees per second
47	Edge	Momentarily true when triggered by Operand A. Operand A is the activation operator [boolean], Operand B (Optional) is the time for the edge to stay active [ms]. After activation, operator will return true until the time in Operand B is reached. If a pure momentary edge is wanted. Just leave Operand B as the default Value: 0 setting.
48	Delay	Delays activation after being triggered. This will return true when Operand A is true, and has been true for the last Operand B [ms].
49	Timer	A simple on - off timer. true for the duration of Operand A [ms]. Then false for the duration of Operand B [ms].
50	Delta	This returns true when the value of Operand A has changed by the value of Operand B or greater within 100ms. ( |ΔA| >= B )
51	Approx Equals (A ~ B)	true if Operand B is within 1% of Operand A.
52	LED Pin PWM	Value Operand A from [0 : 100] PWM / PINIO generation on LED Pin. See LED pin PWM. Any other value stops PWM generation (stop to allow ws2812 LEDs updates in shared modes).
53	Disable GPS Sensor Fix	Disables the GNSS sensor fix. For testing GNSS failure.
54	Mag calibration	Trigger a magnetometer calibration.
55	Set Gimbal Sensitivity	Scales Operand A from [-16 : 15]
56	Override Minimum Ground Speed	When active, sets the minimum ground speed to the value specified in Operand A [m/s]. Minimum allowed value is set in nav_min_ground_speed. Maximum value is 150

Operands

Operand Type	Name	Notes
0	Value	Value derived from value field
1	Get RC Channel	value points to RC channel number, indexed from 1
2	Flight	value points to Flight Parameters table
3	Flight Mode	value points to Flight_Mode table
4	Logic Condition	value points to other logic condition ID
5	Get Global Variable	Value stored in Global Variable indexed by value. GVAR 1 means: value in GVAR 1
5	Programming PID	Output of a Programming PID indexed by value. PID 1 means: value in PID 1
6	Waypoints	value points to the Waypoint parameter table

Flight Parameters

Operand Value	Name	Notes
0	ARM Timer [s]	Time since armed in seconds
1	Home Distance [m]	distance from home in meters
2	Trip distance [m]	Trip distance in meters
3	RSSI
4	Vbat [centi-Volt] [1V = 100]	VBAT Voltage in Volts * 100, eg. 12.1V is 1210
5	Cell voltage [centi-Volt] [1V = 100]	Average cell voltage in Volts * 100, eg. 12.1V is 1210
6	Current [centi-Amp] [1A = 100]	Current in Amps * 100, eg. 9A is 900
7	Current drawn [mAh]	Total used current in mAh
8	GPS Sats
9	Ground speed [cm/s]	Ground speed in cm/s
10	3D speed [cm/s]	3D speed in cm/s
11	Air speed [cm/s]	Air speed in cm/s
12	Altitude [cm]	Altitude in cm
13	Vertical speed [cm/s]	Vertical speed in cm/s
14	Throttle position [%]	Throttle position in %
15	Roll [deg]	Roll attitude in degrees
16	Pitch [deg]	Pitch attitude in degrees
17	Is Armed	Is the system armed? boolean 0/1
18	Is Autolaunch	Is auto launch active? boolean 0/1
19	Is Controlling Altitude	Is altitude being controlled? boolean 0/1
20	Is Controlling Position	Is the position being controlled? boolean 0/1
21	Is Emergency Landing	Is the aircraft emergency landing? boolean 0/1
22	Is RTH	Is RTH active? boolean 0/1
23	Is Landing	Is the aircaft automatically landing? boolean 0/1
24	Is Failsafe	Is the flight controller in a failsafe? boolean 0/1
25	Stabilized Roll	Roll PID controller output [-500:500]
26	Stabilized Pitch	Pitch PID controller output [-500:500]
27	Stabilized Yaw	Yaw PID controller output [-500:500]
28	3D home distance [m]	3D distance to home in meters. Calculated from Home distance and Altitude using Pythagorean theorem
29	CRSF LQ	Link quality as returned by the CRSF protocol
30	CRSF SNR	SNR as returned by the CRSF protocol
31	GPS Valid Fix	Boolean 0/1. True when the GPS has a valid 3D Fix
32	Loiter Radius [cm]	The current loiter radius in cm.
33	Active Control Profile	Integer for the active config profile [1..MAX_PROFILE_COUNT]
34	Battery cells	Number of battery cells detected
35	AGL status [0/1]	Boolean 1 when AGL can be trusted, 0 when AGL estimate can not be trusted
36	AGL [cm]	Integer altitude above The Groud Altitude in cm
37	Rangefinder [cm]	Integer raw distance provided by the rangefinder in cm
38	Active Mixer Profile	Which mixer is currently active (for vtol etc)
39	Mixer Transition Active	Boolean 0/1. Are we currently switching between mixers (quad to plane etc)
40	Yaw [deg]	Current heading (yaw) in degrees
41	FW Land Sate	Integer 1 - 5, indicates the status of the FW landing, 0 Idle, 1 Downwind, 2 Base Leg, 3 Final Approach, 4 Glide, 5 Flare
42	Current battery profile	The active battery profile. Integer [1..MAX_PROFILE_COUNT]
43	Flown Loiter Radius [m]	The actual loiter radius flown by a fixed wing during hold modes, in meters
44	Downlink Link Quality
45	Uplink RSSI [dBm]
46	Minimum Ground Speed [m/s]	The current minimum ground speed allowed in navigation flight modes
47	Horizontal Wind Speed [cm/s]	Estimated wind speed. If the wind estimator is unavailble or the wind estimation is invalid, -1 is returned
48	Wind Direction [deg]	Estimated wind direction. If the wind estimator is unavailble or the wind estimation is invalid, -1 is returned
49	Relative Wind Offset [deg]	The relative offset between the heading of the aircraft and the heading of the wind. 0 indicates flying directly into a headwing. Negative numbers are a left offset. For example, if -20° is shown, turning right will correct towards 0. If the wind estimator is unavailble or the wind estimation is invalid, 0 is returned

FLIGHT_MODE

The flight mode operands return true when the mode is active. These are modes that you will see in the Modes tab. Note: the USER* modes are used by camera switchers, PINIO etc. They are not the Waypoint User Actions. See the Waypoints section to access those.

Operand Value	Name	Notes
0	Failsafe	true when a Failsafe state has been triggered.
1	Manual	true when you are in the Manual flight mode.
2	RTH	true when you are in the Return to Home flight mode.
3	Position Hold	true when you are in the Position Hold or Loiter flight modes.
4	Cruise	true when you are in the Cruise flight mode.
5	Altitude Hold	true when you the Altitude Hold flight mode modifier is active.
6	Angle	true when you are in the Angle flight mode.
7	Horizon	true when you are in the Horizon flight mode.
8	Air	true when you the Airmode flight mode modifier is active.
9	USER 1	true when the USER 1 mode is active.
10	USER 2	true when the USER 2 mode is active.
11	Course Hold	true when you are in the Course Hold flight mode.
12	USER 3	true when the USER 3 mode is active.
13	USER 4	true when the USER 4 mode is active.
14	Acro	true when you are in the Acro flight mode.
15	Waypoint Mission	true when you are in the WP Mission flight mode.

WAYPOINTS

Operand Value	Name	Notes
0	Is WP	Boolean 0/1
1	Current Waypoint Index	Current waypoint leg. Indexed from 1. To verify WP is in progress, use Is WP
2	Current Waypoint Action	true when Action active in current leg. See ACTIVE_WAYPOINT_ACTION table
3	Next Waypoint Action	true when Action active in next leg. See ACTIVE_WAYPOINT_ACTION table
4	Distance to next Waypoint	Distance to next WP in metres
5	Distance from Waypoint	Distance from the last WP in metres
6	User Action 1	true when User Action 1 is active on this waypoint leg [boolean 0/1]
7	User Action 2	true when User Action 2 is active on this waypoint leg [boolean 0/1]
8	User Action 3	true when User Action 3 is active on this waypoint leg [boolean 0/1]
9	User Action 4	true when User Action 4 is active on this waypoint leg [boolean 0/1]
10	Next Waypoint User Action 1	true when User Action 1 is active on the next waypoint leg [boolean 0/1]
11	Next Waypoint User Action 2	true when User Action 2 is active on the next waypoint leg [boolean 0/1]
12	Next Waypoint User Action 3	true when User Action 3 is active on the next waypoint leg [boolean 0/1]
13	Next Waypoint User Action 4	true when User Action 4 is active on the next waypoint leg [boolean 0/1]

ACTIVE_WAYPOINT_ACTION

Action	Value
WAYPOINT	1
HOLD_TIME	3
RTH	4
SET_POI	5
JUMP	6
SET_HEAD	7
LAND	8

Flags

All flags are reseted on ARM and DISARM event.

bit	Decimal	Function
0	1	Latch - after activation LC will stay active until LATCH flag is reset
1	2	Timeout satisfied - Used in timed operands to determine if the timeout has been met

Global variables

CLI

gvar <index> <default value> <min> <max>

Note: Global Variables (GVARs) are limited to integers between negative -32768 and positive 32767.

Programming PID

IPF makes a set of general user PIDFF controllers avaliable for use in your program. These PIDFF controllers are not tied to any roll/pitch/yaw profiles or other controls. The output of these controllers can be used in an IPF program by using the Programming PID operand. The <setpoint value> of the controller is the target value for the controller to hit. The <measurement value> is the measurement of the current value. For instance, <setpoint value> could be the speed you want to go, and <measurement value> is the current speed. P, I, D, and FF values will need to be manually adjusted to determine the appropriate value for the program and controller.

pid <index> <enabled> <setpoint type> <setpoint value> <measurement type> <measurement value> <P gain> <I gain> <D gain> <FF gain>

• <index> - ID of PID Controller, starting from 0
• <enabled> - 0 evaluates as disabled, 1 evaluates as enabled
• <setpoint type> - See Operands paragraph
• <setpoint value> - See Operands paragraph
• <measurement type> - See Operands paragraph
• <measurement value> - See Operands paragraph
• <P gain> - P-gain, scaled to 1/1000
• <I gain> - I-gain, scaled to 1/1000
• <D gain> - D-gain, scaled to 1/1000
• <FF gain> - FF-gain, scaled to 1/1000

Examples

When more than 100 meters away, increase VTX power

When more than 600 meters away, engage return-to-home by setting the matching RC channel

Dynamic THROTTLE scale

logic 0 1 0 23 0 50 0 0 0

Limits the THROTTLE output to 50% when Logic Condition 0 evaluates as true

Set VTX power level via Smart Audio

logic 0 1 0 25 0 3 0 0 0

Sets VTX power level to 3 when Logic Condition 0 evaluates as true

Invert ROLL and PITCH when rear facing camera FPV is used

Solves the problem from https://github.com/iNavFlight/inav/issues/4439

logic 0 1 0 26 0 0 0 0 0
logic 1 1 0 27 0 0 0 0 0

Inverts ROLL and PITCH input when Logic Condition 0 evaluates as true. Moving Pitch stick up will cause pitch down (up for rear facing camera). Moving Roll stick right will cause roll left of a quad (right in rear facing camera)

Cut motors but keep other throttle bindings active

logic 0 1 0 29 0 1000 0 0 0

Sets throttle output to 0% when Logic Condition 0 evaluates as true

Set throttle to 50% and keep other throttle bindings active

logic 0 1 0 29 0 1500 0 0 0

Sets throttle output to about 50% when Logic Condition 0 evaluates as true

Set throttle control to different RC channel

logic 0 1 0 29 1 7 0 0 0

If Logic Condition 0 evaluates as true, motor throttle control is bound to RC channel 7 instead of throttle channel

Set VTX channel with a POT

Set VTX channel with a POT on the radio assigned to RC channel 6

logic 0 1 -1 15 1 6 0 1000 0
logic 1 1 -1 37 4 0 0 7 0
logic 2 1 -1 14 4 1 0 1 0
logic 3 1 -1 31 4 2 0 0 0

Steps:

1. Normalize range [1000:2000] to [0:1000] by substracting 1000
2. Scale range [0:1000] to [0:7]
3. Increase range by 1 to have the range of [1:8]
4. Assign LC#2 to VTX channel function

Set VTX power with a POT

Set VTX power with a POT on the radio assigned to RC channel 6. In this example we scale POT to 4 power level [1:4]

logic 0 1 -1 15 1 6 0 1000 0
logic 1 1 -1 37 4 0 0 3 0
logic 2 1 -1 14 4 1 0 1 0
logic 3 1 -1 25 4 2 0 0 0

Steps:

1. Normalize range [1000:2000] to [0:1000] by substracting 1000
2. Scale range [0:1000] to [0:3]
3. Increase range by 1 to have the range of [1:4]
4. Assign LC#2 to VTX power function

Common Issues / Questions About IPF

One common mistake involves setting RC channel values. To override (set) the value of a specific RC channel, choose "Override RC value", then for operand A choose value and enter the channel number. Choosing "get RC value" is a common mistake, which does something other than what you probably want.

Related Documentation

• JavaScript Programming Guide - Alternative JavaScript-based syntax for programming logic conditions
• Operations Reference - Complete reference for all supported operations in JavaScript
• Timer and Change Detection Examples - Practical examples for time-based patterns