Neural network based algorithms for comprehensive collective axis limit avoidance on rotorcraft

Engineering

• Rotorcraft 100%
• Transients 60%
• Control System 40%
• Flight Control 20%
• Feedback Controller 20%
• Structural Integrity 20%
• Simulation Model 20%
• Exceedance 20%
• Flight Envelope 20%
• Simulation Time 20%
• Dynamic Trim 20%
• Engine Inoperative 20%

Keyphrases

• Torque Prediction 40%
• Response Estimation 20%
• Advanced Prediction 20%
• Excessive Workload 20%
• Transmission Torque 20%
• Maneuvering Capability 20%
• One Engine Inoperative 20%
• Automatic Flight Control System 20%
• Numerical Computing 20%
• Continuous Torque 20%