Genesys Aerosystems HeliSAS with Autopilot (no Beep Trim available) Kit
**PRICE DOES NOT INCLUDE INSTALL LABOR**
The Genesys Aerosystems HeliSAS is a stability augmentation system (SAS) and two-axis
autopilot that provides attitude stabilization and force feedback to the cyclic control for
helicopters with hydraulically assisted flight controls. The system architecture is a parallel design that maintains the integrity of the basic helicopter flight control rods while using electro-mechanical servo actuators that are connected to the helicopter’s flight controls rods with parallel linkage.
The HeliSAS is designed as an attitude-based system that accepts attitude source data using a combination of the installed attitude gyro or digital attitude heading reference system (AHRS) inputs, and motion sensors located in the Flight Control Computer (FCC). The FCC commands the servo actuators to apply small corrections to the cyclic as required to maintain attitude.
Photo Of R44 courtesy By D. Miller - flickr, CC BY 2.0, https://commons.wikimedia.org/w/index.php?curid=87605572
**PRICE DOES NOT INCLUDE INSTALL LABOR**
The Genesys Aerosystems HeliSAS is a stability augmentation system (SAS) and two-axis
autopilot that provides attitude stabilization and force feedback to the cyclic control for
helicopters with hydraulically assisted flight controls. The system architecture is a parallel design that maintains the integrity of the basic helicopter flight control rods while using electro-mechanical servo actuators that are connected to the helicopter’s flight controls rods with parallel linkage.
The HeliSAS is designed as an attitude-based system that accepts attitude source data using a combination of the installed attitude gyro or digital attitude heading reference system (AHRS) inputs, and motion sensors located in the Flight Control Computer (FCC). The FCC commands the servo actuators to apply small corrections to the cyclic as required to maintain attitude.
Photo Of R44 courtesy By D. Miller - flickr, CC BY 2.0, https://commons.wikimedia.org/w/index.php?curid=87605572
**PRICE DOES NOT INCLUDE INSTALL LABOR**
The Genesys Aerosystems HeliSAS is a stability augmentation system (SAS) and two-axis
autopilot that provides attitude stabilization and force feedback to the cyclic control for
helicopters with hydraulically assisted flight controls. The system architecture is a parallel design that maintains the integrity of the basic helicopter flight control rods while using electro-mechanical servo actuators that are connected to the helicopter’s flight controls rods with parallel linkage.
The HeliSAS is designed as an attitude-based system that accepts attitude source data using a combination of the installed attitude gyro or digital attitude heading reference system (AHRS) inputs, and motion sensors located in the Flight Control Computer (FCC). The FCC commands the servo actuators to apply small corrections to the cyclic as required to maintain attitude.
Photo Of R44 courtesy By D. Miller - flickr, CC BY 2.0, https://commons.wikimedia.org/w/index.php?curid=87605572