- the mc pos controller will decrease throttle during the transition
and thus the vehicle will not pick up enough airspeed to complete the
transition

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

to VtolType class

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

- moved methods used to modify channel maximum pwm value to VtolType
class so that the can be shared by the differnt vtol types

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

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

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

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

calculation

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

- more intuitive
- avoids tons of divisions

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

- do not call hrt_elapsed_time since it's expensive
- remove P2 front transition phase (was not even used)

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

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

the mc pos controller handle it for now

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

* revise pitch transition start and actuator_out_1 in transition

* update with new matrix math library

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

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

temporarily use indicated airspeed for transitions so we're consistent with tecs until we move tecs to true airspeed

- use the transition trust when waiting for TECS to kick in
after transition

Conflicts:
	src/modules/vtol_att_control/tailsitter.cpp
	src/modules/vtol_att_control/tiltrotor.cpp
	src/modules/vtol_att_control/vtol_att_control_main.cpp
	src/modules/vtol_att_control/vtol_att_control_main.h
	src/modules/vtol_att_control/vtol_type.h

turning on fw controler during p2 front transiion
simpling the weight for testing
setting output more like fw for transition