Merge Oneloop with rotwing-state and scheduling

[dewagter]

• both use generated autopilot @Dennis-Wijngaarden
• NPS simulator in SI units
• both use same sequence of actuators
• guidance code should be in guidance (make sense, no?)
• direct IDX actuator e.g. actuator_pprz[0]
• weak guidance_indi_get_liftd -> should be in tailsitter
• Add rotorcraft "type" instead of using guidance_indi_hybrid quad plane or tailsitter #3210
• Restore original idea + enhance: command -> failsafe -> actuator #3214
• Make super clean that the order of commands matters
• simulation can go back to using commands directly
• Change order to Real (motors then servos)-Virtual-Passive
• Merge JSBSIM simulators for RW

[tmldeponti]

To Do @tmldeponti

• Oneloop ANDI-INDI switch from actuator_pprz to commands
• Jsbsim NPS adaptation to use commands instead of actuator_pprz
• RW3C airframe with commands instead of actuator pprz
• Rot wing state cleared from Guidance and stabilization INDI references
• Rot wing state, cleaner pitch scheduling definition.
• Made clear what the actuator order is (see airframe RW3C simulation)
• NPS JSBSIM simulation of QUAD in SI units
• Find a way to define for all controllers the number of actuators and type (these numbers can be used to define for loops and efectiveness matrices sizes) see cf42451
• Streamlined NPS with commands
• Started restructuring scheduling effectiveness for rw3c

To Do @dewagter @Dennis-Wijngaarden

• Make sure to move all guidance code to guidance, all stabilization code to stabilization
• Switch from actuator_pprz to commands in your airframe and INDI
• Switch to generated autopilot
• Make sure to use the defined actuator sequence (Real-Virtual-Passive)
• weak guidance_indi_get_liftd should be in tailsitter
• Add rotorcraft "type" instead of using guidance_indi_hybrid quad plane or tailsitter #3210
• Implement the commands based actuator counting method as in the oneloop
• Use only the relevant rows of the effectiveness matrix from the scheduling module in stab and gui
• define max velocity and acceleration in NAV not guidance.

To Do @ALL

• Implement full SI JSBSIM model (a simple one)
• Rot wing effectiveness scheduling cleared of guidance and stabilization INDI references