原文传递
A Control Allocation Technique to Recover From Pilot-Induced Oscillations (CAPIO) Due to Actuator Rate Limiting
| 题名： | A Control Allocation Technique to Recover From Pilot-Induced Oscillations (CAPIO) Due to Actuator Rate Limiting |
| 作者： | Yildiz, Yildiray; Kolmanovsky, Ilya V. |
| 关键词： | allocation；control；pilot；capi；limit；rate；from；command；shift；locator |
| 摘要： | This paper proposes a control allocation technique that can help pilots recover from pilot induced oscillations (PIO). When actuators are rate-saturated due to aggressive pilot commands, high gain flight control systems or some anomaly in the system, the effective delay in the control loop may increase depending on the nature of the cause. This effective delay increase manifests itself as a phase shift between the commanded and actual system signals and can instigate PIOs. The proposed control allocator reduces the effective time delay by minimizing the phase shift between the commanded and the actual attitude accelerations. Simulation results are reported, which demonstrate phase shift minimization and recovery from PIOs. Conversion of the objective function to be minimized and constraints to a form that is suitable for implementation is given. |
| 报告类型： | 科技报告 |
相关文献
- Real-Time Optimization for use in a Control Allocation System to Recover from Pilot Induced Oscillations.
- Adaptive Flight Control for Aircraft Safety Enhancements
- Handling Qualities and Flight Safety Implications of Rudder Control Strategies and Systems in Transport Aircraft.
- Handling Qualities and Flight Safety Implications of Rudder Control Strategies and Systems in Transport Aircraft. Final rept.
- Flight Test Results from the NF-15B Intelligent Flight Control System (IFCS) Project with Adaptation to a Simulated Stabilator Failure
- Deriving an Empirical Model of an Electrohydraulic Actuator System from Frequency Response Data
检索历史
应用推荐
