Cargando…
Aviation Safety and Pilot Control : Understanding and Preventing Unfavorable Pilot-Vehicle Interactions.
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington :
National Academies Press,
1900.
|
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- ""Aviation Safety And Pilot Control""; ""Copyright""; ""Preface""; ""Contents""; ""Executive Summary""; ""THE AIRCRAFT-PILOT COUPLING EXPERIENCE""; ""IMPACT OF NEW TECHNOLOGY""; ""AIRCRAFT-PILOT COUPLING EVENTS AS A CURRENT PROBLEM IN AVIATION""; ""INCREASING AWARENESS""; ""ELIMINATING AIRCRAFT-PILOT COUPLING EVENTS""; ""Management""; ""Design Criteria""; ""Simulation and Flight Tests""; ""INTERIM PRESCRIPTION FOR AVOIDING SEVERE AIRCRAFT-PILOT COUPLING EVENTS""; ""Reduce Category I Pilot-Induced Oscillation Tendencies""; ""Implications for Design of the Effective Aircraft Dynamics""
- ""Suitable Metrics and Criteria""""Minimize Category II and III Pilot-Induced Oscillation Tendencies""; ""Implications for Design of the Effective Aircraft Dynamics""; ""Suitable Metrics and Criteria""; ""Examine the Possibility of Non-Oscillatory Aircraft-Pilot Coupling Events""; ""Conduct Assessments and Evaluations Using Simulators""; ""Implications for Design""; ""Implications for Test Execution""; ""Conduct Flight Evaluations""; ""ALTERNATIVE APPROACHES""; ""1 Aircraft-Pilot Coupling Problems: Definitions, Descriptions, and History ""; ""INTRODUCTION""; ""Initial Concrete Example""
- ""PILOT-VEHICLE CLOSED-LOOP SYSTEM""""NECESSARY CONDITIONS FOR OSCILLATORY AIRCRAFT-PILOT COUPLING EVENTS""; ""HISTORICAL ANTECEDENTS""; ""Aircraft with Conventional Flight Control Systems""; ""Aircraft with Fly-by-Wire Flight Control Systems""; ""STUDY OVERVIEW""; ""Statement of Task and Committee Membership""; ""Study Approach""; ""Report Organization""; ""2 Varieties of Aircraft-Pilot Coupling Experience ""; ""INTRODUCTION""; ""CATEGORIES OF OSCILLATORY AIRCRAFT-PILOT COUPLING EVENTS""; ""Category I: Linear Pilot-Vehicle System Oscillations""
- ""Category II: Quasi-Linear Pilot-Vehicle System Oscillations with Rate or Position Limiting""""Category III: Nonlinear Pilot-Vehicle System Oscillations with Transitions""; ""NONLINEAR, CLIFF-LIKE, PILOT-INVOLVED OSCILLATIONS""; ""Common Cliff Producers""; ""Rate Limiting""; ""Command Path Gain Shaping""; ""NON-OSCILLATORY AIRCRAFT-PILOT COUPLING""; ""TRIGGERS""; ""Environmental Triggers""; ""Vehicle Triggers""; ""Flight Control System-Aircraft Configuration Mismatches""; ""System failures""; ""FCS Mode Shifts""; ""Pilot Triggers""
- ""CASE STUDIES OF RECENT AIRCRAFT-PILOT COUPLING EVENTS IN FLY-BY-WIRE SYSTEMS""""Case 1. Lockheed Martin/Boeing YF-22""; ""Description of Event""; ""Analysis""; ""Post-Event Simulations""; ""Case 2. Boeing 777""; ""Description of Event""; ""Post-Event Flight Test and Simulation""; ""Analysis""; ""Conclusions""; ""Case 3. McDonnell-Douglas C-17""; ""Description of Event""; ""Analysis""; ""Corrective Action""; ""Case 4. Airbus A 320""; ""Description of Event""; ""Analysis""; ""Conclusions""; ""Case 5. Special Considerations for Rotorcraft""