LEADER 05828aam 2200721 450 001 9910808895403321 005 20230120012942.0 010 $a1-4832-9692-X 035 $a(CKB)2670000000585879 035 $a(EBL)1888689 035 $a(OCoLC)898422508 035 $a(SSID)ssj0001266525 035 $a(PQKBManifestationID)11723278 035 $a(PQKBTitleCode)TC0001266525 035 $a(PQKBWorkID)11249638 035 $a(PQKB)11310723 035 $a(MiAaPQ)EBC1888689 035 $a(EXLCZ)992670000000585879 100 $a20150110h19951995 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aAutomatic control in aerospace $eAerospace Control '94 : a postprint volume from the IFAC symposium, Palo Alto, California, USA, 12-16 September 1994 /$fedited by D. B. Schaechter and K. R. Lorell 205 $aFirst edition. 210 1$aOxford, England :$cPergamon,$d1995. 210 4$dİ1995 215 $a1 online resource (447 p.) 225 1 $aIFAC Postprint Volume 300 $aDescription based upon print version of record. 311 $a0-08-042238-1 311 $a1-322-48019-2 320 $aIncludes bibliographical references at the end of each chapters and index. 327 $a""Front Cover""; ""Automatic Control in Aerospace (Aerospace Control '94)""; ""Copyright Page""; ""Table of Contents""; ""IFAC SYMPOSIUM ON AUTOMATIC CONTROL IN AEROSPACE 1994""; ""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"" 327 $a""2 MATHEMATICAL MODELS""""3 OPTIMIZATION METHOD""; ""4 COMPUTATIONAL STUDY""; ""5 CONCLUSIONS""; ""6 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"" 327 $a""5. ASSESSMENT""""6. CONCLUSIONS""; ""7. ACKNOWLEDGMENT""; ""8. REFERENCES""; ""CHAPTER 5. OPTIMAL GUIDANCE OF A SOLAR SAIL SPACECRAFT TO THE SUN-EARTH L2 POINT""; ""1. INTRODUCTION""; ""2. 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"" 327 $a""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 CONTROL""; ""4. 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"" 327 $a""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. RESULTS""; ""8. 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"" 327 $a""5. PLANNING OF LANDING SEQUENCES AND SCHEDULES"" 330 $aAn important, successful area for control systems development is that of state-of-the-art aeronautical and space related technologies. Leading researchers and practitioners within this field have been given the opportunity to exchange ideas and discuss results at the IFAC symposia on automatic control in aerospace. The key research papers presented at the latest in the series have been put together in this publication to provide a detailed assessment of present and future developments of these control system technologies. 410 0$aIFAC Postprint Volume 606 $aAirplanes$xControl systems$vCongresses 606 $aAirplanes$xAutomatic control$vCongresses 606 $aSpace vehicles$xControl systems$vCongresses 606 $aSpace vehicles$xAutomatic control$vCongresses 615 0$aAirplanes$xControl systems 615 0$aAirplanes$xAutomatic control 615 0$aSpace vehicles$xControl systems 615 0$aSpace vehicles$xAutomatic control 676 $a629.132/6 676 $a629.1326 702 $aSchaechter$b D. B. 702 $aLorell$b K. R. 712 02$aInternational Federation of Automatic Control. 712 12$aIFAC Symposium on Automatic Control in Aerospace$f(1994 :$ePalo Alto, California) 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910808895403321 996 $aAutomatic control in aerospace$94037120 997 $aUNINA