joe@tech-mp
Dec 01, 2005, 12:19 PM
Here is the problem:
In a tandem helicopter (Chinook type), the yaw (rudder) is controlled by differential cyclic on the roll axis. To yaw left, the front rotor tilts left and the rear rotor tilts right. So, the yaw axis on a tandem is controlled by the roll axis. As many of you know, roll control sense does not change whether the model is right side up (RSU) or up side down (USD) like rudder and elevator. When a tandem is flying RSU everything is fine, the yaw gyro sense is correct. When flying USD the controls and gyro (yaw) are inverted but the roll axis is the same. The result is reversed rudder control with the gyro correcting in the wrong direction. Currently, this is a barrier that limits tandem 3-D flying.
Here are some potential solutions already on the table:
1. Use a pilot controlled invert switch on the Tx. - Old school way of handling it.
2. Change the yaw signal polarity based on Tx collective pitch position - This has been experimented with and had
limited success. The stick position does not exactly follow the lift vectors of the rotors.
3. Use a sensor or group of sensors to accurately detect the RSU or USD position.
I like the number 3 approach the best. The sensor(s) would be inputs to a tandem mixer (TH-2) which would process the signals and apply the polarity corrections. The sensors must work both outside and indoors with artificial lighting. Also, they must handle the effects of gravity and centrifugal force from any 3-D flight manuver.
Any Ideas would be appreciated.
Joe
In a tandem helicopter (Chinook type), the yaw (rudder) is controlled by differential cyclic on the roll axis. To yaw left, the front rotor tilts left and the rear rotor tilts right. So, the yaw axis on a tandem is controlled by the roll axis. As many of you know, roll control sense does not change whether the model is right side up (RSU) or up side down (USD) like rudder and elevator. When a tandem is flying RSU everything is fine, the yaw gyro sense is correct. When flying USD the controls and gyro (yaw) are inverted but the roll axis is the same. The result is reversed rudder control with the gyro correcting in the wrong direction. Currently, this is a barrier that limits tandem 3-D flying.
Here are some potential solutions already on the table:
1. Use a pilot controlled invert switch on the Tx. - Old school way of handling it.
2. Change the yaw signal polarity based on Tx collective pitch position - This has been experimented with and had
limited success. The stick position does not exactly follow the lift vectors of the rotors.
3. Use a sensor or group of sensors to accurately detect the RSU or USD position.
I like the number 3 approach the best. The sensor(s) would be inputs to a tandem mixer (TH-2) which would process the signals and apply the polarity corrections. The sensors must work both outside and indoors with artificial lighting. Also, they must handle the effects of gravity and centrifugal force from any 3-D flight manuver.
Any Ideas would be appreciated.
Joe