File change tracker #72
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This is a new battery type which reads data of 2 battery over I2C using an ADC I2C Extender.
Addition of Battery Type.
Currently if the CAN data is stopped receiving AP_Periph will still remain in the last known ARM state. Changes Made: AP_Periph will Disarm if 1) A specific disarm command is received 2) no arming command and no ESC command receive for DISARM_DELAY period.
Implementation for Hirth. Base class - AP_EFI WIP: Log functional
includes updates for TCA9554 pin mapping
Added driver for APD HVPro Telemetry feedback. Will be only compiled if added in hwdef
Added AP_ESC_HVPro and also removed ADSB support.
OV3-396 AP_Perip: AP_ESC_APDHVPro200 : Data type modified OV3-396 AP_ESC_APDHVPro: Current, Voltage and Temperature values are changed from Int to Float OV3-396 AP_ESC_APDHVPro: Add voltage calibration code OV3-522 APDHVPro temporary CURRENT_COEFFICIENT OV3-493 AP_ESC_Telem : revert current coef to 12.5
…meout ARM Timeout: is changed to 2000 as it is now only scanning ARM signal which is arriving at 1Hz ESC timeout: Timeout defaults to 200ms. Timeout can be disabled by setting parameter to 0. Timeout should be configured to be able to handle at small number of missed packets.
ARM _Monitoring: dropped to be also cleared at ESC signal received ESC_Timeout: Fixes a periph continuing to drive an ESC to an output when the esc_rawcommand packets are lost
From now we don't need to edit the print command in AP_Periph .cpp
Have added a new variable "error_status" which is gets its value for HVPro. This value is sent over can "ESC_Status" pkt replacing "error_count"
extract error_count pkt to error_status
this allows for testing of a fwd motor or control surfaces while not allowing for VTOL ESCs to run. This makes CAN actuators behave the same as direct PWM actuators
this sets up the vwd integrator more reasonably when we are in POSITION1 stage of VTOL landing. We need to have enough throttle to cope with a headwind, but want it lower when we are at or above our target closing speed so can minimise the amount of pitch up This also makes the landing_desired_closing_velocity() consistent with the landing speed used in approach, using average of airspeed min and cruise speed if TECS_LAND_ARSPD is not set The target airspeed for TECS during airbraking is now set to ARSPD_FBW_MIN, on the basis we are trying to slow down to min speed, and we have VTOL support which should prevent a stall. To cope with a high headwind where ARSPD_FBW_MIN is below the headwind we now check for too low achieved closing speed and switch to POSITION1 which can use vfwd to get to the landing location
1. port->begin() handled 2. if ( > ESC_PACKET_SIZE * 2) then packets are discarded 3. last_read_ms is updated only if parse is successful 4. divide by '0' is handled 5. proceed only if fletcher checksum succeeds
Implemented CANH log section which includes - Health, Uptime and Delta of CAN devices Update libraries/AP_UAVCAN/AP_UAVCAN_DNA_Server.h Co-authored-by: Jono453 <[email protected]>
Cherry picked from OV3-415
Cherry picked From: OV3-415
just sums the values of the bytes in a buffer and returns that sum modulus 256
LOG_NODE_STATUS changed to ENABLE_STATS which is bit 8
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