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inav/docs/Programming Framework.md
Pawel Spychalski (DzikuVx) 426d21a9fc Cleanup
2020-07-23 10:47:43 +02:00

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INAV Programming Framework

INAV Programming Framework (abbr. IPF) is a mechanism that allows to evaluate cenrtain flight parameters (RC channels, switches, altitude, distance, timers, other logic conditions) and use the value of evaluated expression in different places of INAV. Currently, the result of LCs can be used in:

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

INAV Programming Framework coinsists of:

  • Logic Conditions - each Logic Condition can be understood as a single command, a single line of code
  • Global Variables - variables that can store values from and for LogiC Conditions and servo mixer

IPF can be edited using INAV Configurator user interface, of via CLI

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 Evaluates false if false or 0
2 GREATER_THAN
3 LOWER_THAN
4 LOW true if <1333
5 MID true if >=1333 and <=1666
6 HIGH true if >1666
7 AND
8 OR
9 XOR
10 NAND
11 NOR
12 NOT
13 STICKY Operand A is activation operator, Operand B is deactivation operator. After activation, operator will return true until Operand B is evaluated as true
14 ADD Add Operand A to Operand B and returns the result
15 SUB Substract Operand B from Operand A and returns the result
16 MUL Multiply Operand A by Operand B and returns the result
17 DIV Divide Operand A by Operand B and returns the result
18 GVAR SET Store value from Operand B into the Global Variable addressed by Operand B. 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 GVAR INC Increase the GVAR indexed by Operand A with value from Operand B
20 GVAR DEC Decrease the GVAR indexed by Operand A with value from Operand B
21 IO PORT SET 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 to arm on any angle even without GPS fix
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

Operands

Operand Type Name Notes
0 VALUE Value derived from value field
1 RC_CHANNEL value points to RC channel number, indexed from 1
2 FLIGHT value points to flight parameter table
3 FLIGHT_MODE value points to flight modes table
4 LC value points to other logic condition ID
5 GVAR Value stored in Global Variable indexed by value. GVAR 1 means: value in GVAR 1

FLIGHT

Operand Value Name Notes
0 ARM_TIMER in seconds
1 HOME_DISTANCE in meters
2 TRIP_DISTANCE in meters
3 RSSI
4 VBAT in Volts * 10, eg. 12.1V is 121
5 CELL_VOLTAGE in Volts * 10, eg. 12.1V is 121
6 CURRENT in Amps * 100, eg. 9A is 900
7 MAH_DRAWN in mAh
8 GPS_SATS
9 GROUD_SPEED in cm/s
10 3D_SPEED in cm/s
11 AIR_SPEED in cm/s
12 ALTITUDE in cm
13 VERTICAL_SPEED in cm/s
14 TROTTLE_POS in %
15 ATTITUDE_ROLL in degrees
16 ATTITUDE_PITCH in degrees
17 IS_ARMED boolean 0/1
18 IS_AUTOLAUNCH boolean 0/1
19 IS_ALTITUDE_CONTROL boolean 0/1
20 IS_POSITION_CONTROL boolean 0/1
21 IS_EMERGENCY_LANDING boolean 0/1
22 IS_RTH boolean 0/1
23 IS_WP boolean 0/1
24 IS_LANDING boolean 0/1
25 IS_FAILSAFE boolean 0/1

FLIGHT_MODE

Operand Value Name Notes
0 FAILSAFE
1 MANUAL
2 RTH
3 POSHOLD
4 CRUISE
5 ALTHOLD
6 ANGLE
7 HORIZON
8 AIR

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 reseted

Examples

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 Thhrottle 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 Thhrottle 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