Development of a Virtual Ground Testing Model for Aerospace Electromechanical Actuator Design Performance Evaluation

Engineering

• Actuator 100%
• Dynamic Model 33%
• Simplifies 16%
• Nonlinearity 16%
• Actuator System 16%
• Flight Control 16%
• Test Result 16%
• Performance Requirement 16%
• Testing Method 16%
• Servomotors 16%
• Improve Efficiency 16%
• Performance Parameter 16%
• Performance Indicator 16%
• Aerospace Vehicle 16%
• Cost Efficiency 16%
• Maintainability 16%
• Mechanical Component 16%
• Elastic Stiffness 16%
• Rapid Acquisition 16%
• Mechanical Transmission 16%
• Motor Controller 16%