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Flight control of unmanned rotorcrafts for enhanced situational awareness /
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Hauppauge, N.Y. :
Nova Science Publishers, Inc.,
2014.
|
| Colección: | Engineering tools, techniques and tables.
Robotics research and technology. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- FLIGHT CONTROL OF UNMANNED ROTORCRAFTS FOR ENHANCED SITUATIONAL AWARENESS; FLIGHT CONTROL OF UNMANNED ROTORCRAFTS FOR ENHANCED SITUATIONAL AWARENESS; Library of Congress Cataloging-in-Publication Data; Contents; Preface; Chapter 1: Flight Control of Miniature Helicopter; 1.1. A Mathematical Model of an UAV; 1.2. Simulation Results for; Control System; 1.2.1. Example 1; 1.2.2. Example 2; 1.2.3. Example 3; 1.2.4. Example 4; 1.2.5. Example 5; 1.2.6. Example 6; Chapter 2: Flight Control of an Intermediate Helicopter; 2.1. A Mathematical Model of an UAV; 2.2. Control System.
- 2.3. Simulation Results for Control SystemChapter 3: Flight Control of Light Coaxial Rotor/Ducted Fan UAV; 3.1. A Mathematical Model of an UAV; 3.2. Simulation Results for Control System; 3.3. A Mathematical Model of a Two-Rate System; 3.4. Simulation Results for a Two-Rate Control System; 3.5. A Mathematical Model of Three-Rate System; 3.6. Simulation Results for Three-Rate Control System; Chapter 4: Flight Control of Trirotor Mini-UAV; 4.1. A Mathematical Model of an UAV; 4.2. Control System with Controls of Separate Thrusts.
- 4.3. Simulation Results for Control System with Controls of Separate Thrusts4.4. Control System with Control of Collective Thrust; 4.5. Simulation Results for Control System with Control of Collective Thrust; Chapter 5: Flight Control of Mini-VTAV; 5.1. A Mathematical Model of an UAV; 5.2. Control System; 5.3. Simulation Results for Control System; 5.4. A State-Space Model of an UAV; 5.5. Simulation Results for LQG Control System; 5.6. Simulation Results for Neural Network Control System; 5.7. A Mathematical Model of Two-Rate System; 5.8. Simulation Results for Two-Rate LQG Control System.
- Chapter 6: Flight Control of Quadrotor Mini-UAV6.1. A Mathematical Model of an UAV; 6.2. Control System with Controls of Separate Thrusts; 6.3. Simulation Results for Control System with Controls of Separate Thrusts; 6.4. Control System with Control of Collective Thrust; 6.5. Simulation Results for Control System with Control of Collective Thrust; Chapter 7: Flight Control of X4-Flyer Mini-UAV; 7.1. A Mathematical Model of an UAV; 7.2. Control System with Controls of Separate Thrusts; 7.3. Simulation Results for Control System with Controls of Separate Thrusts.
- 7.4. Control System with Control of Collective Thrust7.5. Simulation Results for Control System with Control of Collective Thrust; Chapter 8: Flight Control of an Eight-Rotor Mini-UAV; 8.1. A Mathematical Model of an UAV; 8.2. Control System with Controls of Separate Thrusts; 8.3. Simulation Results for Control System with Controls of Separate Thrusts; 8.4. Control System with Control of Collective Thrust; 8.5. Simulation Results for Control System with Control of Collective Thrust; References; Author's Contact Information; Index.