* FW actuators fully on the entirety of front and back transition
* back transition ramp up to full MC weight half way through back transition
* increase maximum front and back transition times
* navigator don't reset transition altitude
When a FW/VTOL system detects a missing airspeed sensor, it produces an error message.
This patch uses the new relevant URLs in the PX4 documentation.
Fixes#4549
For the process usage: we need to measure over a certain period of time,
then we can use the results. To avoid blocking, this does:
- after log is started, initialze the load counters, then one second later
add the results to the log
- after disarming: continue logging for one more second, then add the process
load to the log and stop logging.
- to avoid a delay, 'logger stop' will stop immediately and not log
postflight process usage.
perf_counters is read from and written to by different threads and thus
requires synchronization. Without it we risk accessing invalid memory.
There are still remaining issues (see comment in code), they will not lead
to a crash however.
Instead of printing to an fd, this prints to a buffer and calls a callback
for each line. To avoid code duplication, the print_load has been refactored
to print to a buffer first, then print to an fd. The overhead is not
noticable, and the behavior of print_load is unchanged.
what could have gone wrong before? A scheduling switch during the printload
could have led to a task exit, rendering the tcb invalid. After switching
back, printload would access invalid memory.
This keeps the sched_lock() section as small as possible, just grabbing the
tcb variables we need.
Beat Küng
ChristophTobler
Hamish Willee
Daniel Agar
Dennis Shtatnov
Sander Smeets
Jonathan Lee
Mohammed Kabir
Lorenz Meier
bharath374
FantasyJXF