tested on at least 5 different vehicles, including AeroFC. The values
should be conservative, good setups (with low vibrations) can increase
these values even further.

increasing IMU_GYRO_CUTOFF allows for better tuning gains (increased P).

LTEST_MODE is defined in landing_target_estimator and required by
local_position_estimator.

Required by Navigator.

reduces RAM usage by 1.3KB

- make the selected parameter a template argument. This
  enables type-checking at compile-time.
- move things to src/platforms.
  This provides consistent includes with ModuleBase
- add ModuleParams base class (replaces Block & SuperBlock)
- drop the Block* prefix from the class names

Generates an enum with all params & additional type information for static
type checking

The generated public param header is required to build the modules using
the new BlockParam classes.

Fix: Increase pwmsim module stack by 100 bytes again because load_mon was giving warning about low stack

https://github.com/PX4-NuttX/nuttx/commit/efc3d9e92bd10623ab3025f012fd7d481e1a7267

The mode change was not necessary and in fact caused the chip to not update the registerfile resulting in MAG timeouts

On kinetis, the TPM_STATUS_TOF was used to detect missed interrupts for
PPM decoding. However this was not correct, because the TOF bit was set on
each timer overflow. This happened regularly after every 64ms interval,
which meant that most PPM frames were just discarded.

I have not found any equivalent register/solution that is used on STMF4,
so this just removes the TOF handling. However there is now no way to
detect missed edges/interrupts!

Before, the RC channel was published as fast as the fmu was running
(around 200Hz in unarmed state).

And fix code style.

   Allow whoami of fxos8701cq and fxos8700cq

In the stm32f7 the configuration variable for SD card with DMA changed from CONFIG_STM32_SDIO_DMA to CONFIG_STM32F7_SDMMC_DMA
the maximum clock speed of 16MHz can now be achieved.

Signed-off-by: Roman <bapstroman@gmail.com>

* ecl: attitude_fw update
- move angular rate limits to body angular rates
- handle rattitude/acro vs attitude mode rate limits

- the main idea is to prevent airspeed less systems to stall after a
transition

Signed-off-by: Roman <bapstroman@gmail.com>