Currently if you configure a battery capacity the battery library calculates a remaining flight time and you by default get an RTL when the flight time - return time is running out.
Since the state of charge threshold based battery failsafes `COM_LOW_BAT_ACT` are disabled by default I was asked to also disable the flight time based failsafe to be consistent.
* Add tflm to px4 with module
- Add TensorFlow Lite Micro(TFLM) as a library in px4
- Make a module that uses neural network inference for control, which uses TFLM for inference
- Make board config files for PX4 with neural module
* Added neural flight mode
* Add posibility to read of inference times
* Fix comments from review:
- Switch ssh link to https link in submodule
- Remove mc_nn_control from startup
* Add tflm to px4 with module
- Add TensorFlow Lite Micro(TFLM) as a library in px4
- Make a module that uses neural network inference for control, which uses TFLM for inference
- Make board config files for PX4 with neural module
* Added neural flight mode
* Add posibility to read of inference times
* Remove auto start
* Add logging from neural control module
* Fix automatic startup to only be when module is included
* Switch to flight mode registration
* Add docs
* Change min/max/coeff to actual parameters
* add figures to neural network docs
* Switch to e2e network
* Remove toolchain changes and replace with instructions in docs
* Get ready for merge after toolchain upgrade
* switch back to submodule
* Try to figure out cmake
* Get CI working with new toolchain
* Remove fork dependency
* Finalize PR
* fix toolchain inclusion
* Fix ctype_base.h include
* Cleanup includes for TFLM
* Remove redundant std
* Update FW module names in board files
* Fix docs
* Remove cstdlib copy
* Copy header from nuttx
* Prettier, markup, layout
* NeuralControl.msg - update uorb comments to current standard
* Add description to neural topic
* Fix typo
* Typo
* TFLM and Module utitlities
* Neural networks top level
* Update docs
* Add manual control
* Update docs
* Revert the manual control attempt
* Update docs/en/advanced/nn_module_utilities.md
* Add posibility to set trajectory setpoint with manual control
---------
Co-authored-by: Pedro Roque <padr@kth.se>
Co-authored-by: Hamish Willee <hamishwillee@gmail.com>
Co-authored-by: Ramon Roche <mrpollo@gmail.com>
* rft: clean merge to PX4
* fix: formatting
* fix: extra line
* fix: moved submarine out of "is_ground_vehicle", added proper check for center-throttle
* feat: updated gazebo models to include bluerov update
* fix: use 'is_uuv_vehicle', remove FW_MM/LLC from uuv build
* fix: added saturation to thrust and torque messages via param
* doc: updated parameters documentation for uuv
* fix: formatting
* feat: matching hardware reference
* fix: thrusters kg
* rft: removed commented lines
* fix: update gz reference given hw setup
* fix: hardware references
* fix: recommendations
* fix: updated settings to match hardware
* rft: check only for fixed and rotary wing for high throttle
Co-authored-by: Daniel Agar <daniel@agar.ca>
* fix: commit oupsie
* fix: format
* rft: remove is_uuv
* fix: hw parameters, uuv build target for v6x
* feat: added support for D-pad attitude changes in stabilized position control
* fix: position setpoint update and parametrized trajectory age and att change
* fix: format
* fix: removed duplicated call to check_validity_setpoint
* fix: setpoint update on arming logic
* fix: setpoint initialization for stabilized mode
---------
Co-authored-by: Daniel Agar <daniel@agar.ca>
* rft: initial merging of controllers for spacecraft vehicles
* feat: rate controller nominal
* feat: spacecraft tooling for commander and VehicleStatus
* feat: spacecraft tooling for commander and VehicleStatus
* fix: format
* fix: format
* fix: remove iostream
* fix: remove iostream
* feat: spacecraft attitude control and minor refactoring of params
* feat: add position controller
* fix: format
* fix: moved trajectories to new message, removed derivative filters
* fix: format
* fix: removed extra newline
* fix: spacecraft allocation builds
* feat: add thrusters to effectivenes, add spacecraft build to cmake, clean comments
* feat: required changes for allocation
* feat: thruster simulation interface
* fix: update maximum and minimums
* fix: format
* fix: added newline at the end of spacecraft actuator effectiveness
* feat: configurable board pwm freq from Kconfig
* feat: mavlink compliant spacecraft definition
* feat: add orbiter to define
* boards: Increase TELEM2 rx buffer size for DDS over serial use-case (ARK Jetson)
feat: spacecraft tooling for commander and VehicleStatus
fix: format
fix: remove iostream
feat: mavlink compliant spacecraft definition
* feat: add orbiter to define
* feat: add orbiter to define
* fix: change mav_type to new spacecraft orbiter enum value
* fix: build issue
* feat: update mavlink
* feat: update mavlink to latest master with spacecraft
* feat: update mavlink
* feat: update mavlink to latest
* feat: cleanup and synchronization with new mavlink vehicle definition
* fix: get away without specifying spacecraft vehicle
* fix: removed unnecessary definition
* fix: format
* feat: cmake variant for spacecraft
* feat: proper mav_type and rc init
* fix: removed dart from build system
* add: thrusters to actuator type
* rft: reordering actuator type
* rft: initial merging of controllers for spacecraft vehicles
* feat: rate controller nominal
* fix: format
* feat: spacecraft attitude control and minor refactoring of params
* feat: add position controller
* fix: format
* fix: moved trajectories to new message, removed derivative filters
* fix: format
* fix: removed extra newline
* fix: spacecraft allocation builds
* feat: add thrusters to effectivenes, add spacecraft build to cmake, clean comments
* feat: required changes for allocation
* feat: thruster simulation interface
* fix: update maximum and minimums
* fix: format
* fix: added newline at the end of spacecraft actuator effectiveness
* feat: configurable board pwm freq from Kconfig
* feat: add orbiter to define
* feat: cleanup and synchronization with new mavlink vehicle definition
* fix: get away without specifying spacecraft vehicle
* fix: conflicts
* fix: format
* fix: remove duplicate entry
* rft: remove Kconfig changes
* rft: revert main Kconfig
* rft: revert main kcoonfig on platforms
* rft: remove changes to board PWm (go on another PR)
* rft: revert changes to commander (main is correct)
* fix: extra char on commander_helper
* rft: removed extra spaces
* rft: moved effectiveness to spacecraft
* fix: spacecraft effectiveness
* fix: extra space
* feat: preliminary version, still using thrusters
* rft: initial pipeline on PX4 side with rotors instead of thrusters
* feat: add atmos model
* feat: spacecraft with rotor pipeline tested, working
* feat: update gz
* rft: removed thruster interfaces
* fix: format
* fix: remove control allocation
* fix: thruster normalization
* fix: format
* fix: nuttx version
* fix: clang tidy error
* feat: updated gz to add atmos model
* fix: update gz
* fix: update mavlink
* fix: remove friend class from allocation lib
* fix: remove actuator_outputs/motors
---------
Co-authored-by: Alexander Lerach <alexander@auterion.com>
* Added the ranges for the new ARK Murata IMUs and added the logic to the driver to handle it
* Ran make format
* sch16t fix COMP_ID
* Revert "sch16t fix COMP_ID"
This reverts commit 38bf02bc8616490a37a57257938086b8e8d5fa0f.
* sch16t add production k10 id
* Added B13 as REV_1
---------
Co-authored-by: Alex Klimaj <alex@arkelectron.com>
According to the mavlink spec we should be publishing the home attitude
as a quaternion rather than just the yaw/heading.
Additionally, this allows setting the landing roll and pitch angle using
DO_SET_HOME (this yet needs to go into the MAVLink spec though).
This time including the message versioning and translation.
Previously, when switching from a goto setpoint into a mode that publishes
trajectory_setpoint, the previous goto setpoint was still used for 500ms,
which then caused a setpoint jump.
This change makes sure that when a trajectory_setpoint is received, any
existing goto setpoint is marked as invalid immediately.
There was a race condition: for example when an external mode disabled
failsafe deferring, that then triggered a failsafe, while the mode executor
immediately sends a command (to e.g. switch modes).
In that case the failsafe got triggered but the mode switch was still
allowed.
This was because of the processing ordering:
- mode updates (and propagating the failsafe_action_active state)
- failsafe updates
- command handling
This patch makes sure failsafe_action_active is set immediately after
updating the failsafes.
Previously, when deferring was active and e.g. RC loss was triggered, and
RC regained, the action was not cleared, as the RC loss action only clears
on mode switch/disarm (when set to RTL for example).
When deferring was then disabled, the RC loss failsafe would still trigger.
This changes the behavior to immediately remove those actions when
deferring is active.
It also ensures to reset the Hold delay when deferring is disabled and no
failsafe is being deferred.
Silvan