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Automatic control in aerospace : Aerospace Control '94 : a postprint volume from the IFAC symposium, Palo Alto, California, USA, 12-16 September 1994 /
An important, successful area for control systems development is that of state-of-the-art aeronautical and space related technologies. Leading researchers and practitioners within this field have been given the opportunity to exchange ideas and discuss results at the IFAC symposia on automatic contr...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
Oxford ; New York :
Published for the International Federation of Automatic Control by Pergamon,
1995.
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| Edición: | First edition. |
| Colección: | IFAC Postprint Volume.
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Automatic Control in Aerospace (Aerospace Control '94); Copyright Page; IFAC SYMPOSIUM ON AUTOMATIC CONTROL IN AEROSPACE 1994; Table of Contents; CHAPTER 1. OPTIMAL MULTI-CRITERIA AEROASSISTED ORBITAL TRANSFER TRAJECTORIES; 1. INTRODUCTION; 2. MATHEMATICAL MODEL; 3. MULTI-CRITERIA TRAJECTORY OPTIMIZATION; 4. THE AEROASSISTED ORBITAL TRANSFER PROBLEM; 5. RESULTS AND DISCUSSION; 6. CONCLUSIONS; Acknowledgments; 7. REFERENCES; CHAPTER 2. ROCKET ASCENT WITH HEAT-FLUX AND SPLASH DOWNCONSTRAINTS; 1 INTRODUCTION; 2 MATHEMATICAL MODELS; 3 OPTIMIZATION METHOD; 4 COMPUTATIONAL STUDY.
- 5 conclusions6 references; chapter 3. hierarchical modeling approach in aircraft trajectory optimization; 1. introduction; 2. mathematical modeling; 3. dynamic-model structure; 4. hierarchical optimization; 5. numerical results; conclusions; acknowledgements; references; chapter 4. nonlinear analysis and design of shuttle-type entry guidance; 1. introduction; 2. guidance problem formulation; 3. guidance laws; 4. stability and performance; 5. assessment; 6. conclusions; 7. acknowledgment; 8. references; chapter 5. optimal guidance of a solar sail spacecraft to the sun-earth l2 point.
- 1. introduction2. problem definition; 3. open-loop trajectory; 4. guidance; 5. conclusions; 6. references; chapter 6. adaptive wing camber optimization: a periodic perturbation approach; 1. introduction; 2. problem formulation; 3. a periodic perturbation extremasearching technique: the working principle; 4. practical implementation of the algorithm: equivalent circuit and design; 5. application to active camber optimization; 6. concluding remarks; 7. references; chapter 7. parameter robust flight control systemfor a flexible aircraft; 1. introduction; 2. mixed control.
- 3. parameter robust mixed control4. performance requirement; 5. application; 6. conclusion; 7. references; chapter 8. non-smooth resonance control of complex bifurcations in aircraft flight; 1. introduction; 2. normal forms and averaging reduction methods; 3. estimation of residual terms; 4 . resonance stabilization; 5. analysis and control of complex bifurcations of an aircraft model; 6. conclusion; 7. references; chapter 9. high angle of attack velocity vector rolls; 1. introduction; 2. approach; 3. modeling; 4. qft overview; 5. attack on nonlinearities and uncertainty; 6. controller design.
- 7. results8. conclusions; 9. references; chapter 10. a route oriented planning and control concept for efficient flight operations at busy airports; 1. introduction; 2. current airport operations; 3. concept description; 4. design algorithms; 5. planning of landing sequences and schedules; 6. generation of speed control advisories; 7. operational analysis results; 8. summary; 9. references; chapter 11. model based vision for aircraft position determination; i. introduction; ii. preliminaries; iii. point sensitivity; iv. sensitivity during landing; v. error correction; vi. conclusions.