Rudder Pedal Shaker
Posted: 16 Nov 2022, 05:56
The Harrier has a RPS system, or rudder pedal shaker, which I think it is relatively unique to the Harrier. It was developed to warn the pilot in slow speeds during hover or transition to or out of hover, from excessive sideslip. If the sideslip becomes to great, it can result in loss of control and a crash. Early AV-8A's did not have this but it was added in the late 70's. The AV-8B also has the SAAHS which helps keep the aircraft stable and is less prone to the excessive sideslip but it could still happen. Anyway, the mission computer with activate the RPS when one of the following conditions occur when lateral acceleration is 0.6G or greater and any of the following conditions exist:
* Gear down and STOL flaps selected
* Gear down and Flaps set to Cruise or Auto and speed less than 0.3 mach
* Gear up, STOL flaps, speed less than 0.3 mach
* Nozzles greater than 10 degrees down
When this happens, the mission computer switches on an electric DC motor with an eccentric weight on the pedal that should be pushed to correct for the sideslip, which causes it to shake.
This isn't modeled in the Razbam Harrier, but I figured out that I can probably replicate it using Dcs-Bios, an Arduino, and 2 vibration motors. From Dcs-Bios I can read the value of the slip ball. I can't read the value of lateral acceleration but I wonder if I could probably calculate it using other values such as AOA, airspeed, lat and lon (and difference based on delta over time), etc. I just ordered a pack of vibration motors from Amazon for $10. The plan is to 3d print a bracket to hold a motor and mount it to the backside of each pedal. The Arduino will switch on the motors when needed, possibly via relay to protect against the current draw of the motor. Alternatively I could use flyback diodes and transistors. Should be a fun little project. There is also a RPS test switch which I can read that should turn on the motors when pressing full rudder while taxing.
Edit: I keep forgetting that the Harrier has a weather vane on the nose specifically to tell the mission computer the angle of side slip. I need to see if the position of that weather vane is readable by dcs-Bios.
* Gear down and STOL flaps selected
* Gear down and Flaps set to Cruise or Auto and speed less than 0.3 mach
* Gear up, STOL flaps, speed less than 0.3 mach
* Nozzles greater than 10 degrees down
When this happens, the mission computer switches on an electric DC motor with an eccentric weight on the pedal that should be pushed to correct for the sideslip, which causes it to shake.
This isn't modeled in the Razbam Harrier, but I figured out that I can probably replicate it using Dcs-Bios, an Arduino, and 2 vibration motors. From Dcs-Bios I can read the value of the slip ball. I can't read the value of lateral acceleration but I wonder if I could probably calculate it using other values such as AOA, airspeed, lat and lon (and difference based on delta over time), etc. I just ordered a pack of vibration motors from Amazon for $10. The plan is to 3d print a bracket to hold a motor and mount it to the backside of each pedal. The Arduino will switch on the motors when needed, possibly via relay to protect against the current draw of the motor. Alternatively I could use flyback diodes and transistors. Should be a fun little project. There is also a RPS test switch which I can read that should turn on the motors when pressing full rudder while taxing.
Edit: I keep forgetting that the Harrier has a weather vane on the nose specifically to tell the mission computer the angle of side slip. I need to see if the position of that weather vane is readable by dcs-Bios.