000771384 000__ 04675cam\a2200529Mi\4500 000771384 001__ 771384 000771384 005__ 20230306142604.0 000771384 006__ m\\\\\o\\d\\\\\\\\ 000771384 007__ cr\un\nnnunnun 000771384 008__ 170104s2016\\\\sz\\\\\\o\\\\\000\0\eng\d 000771384 019__ $$a967655955$$a967769874 000771384 020__ $$a9783319415086$$q(electronic book) 000771384 020__ $$a3319415085$$q(electronic book) 000771384 020__ $$z9783319415062 000771384 020__ $$z3319415069 000771384 035__ $$aSP(OCoLC)ocn967683803 000771384 035__ $$aSP(OCoLC)967683803$$z(OCoLC)967655955$$z(OCoLC)967769874 000771384 040__ $$aYDX$$beng$$cYDX$$dN$T$$dIDEBK$$dEBLCP$$dGW5XE$$dN$T 000771384 049__ $$aISEA 000771384 050_4 $$aTL790 000771384 050_4 $$aQA1-939 000771384 08204 $$a629.4$$223 000771384 08204 $$a510 000771384 24500 $$aSpace engineering$$h[electronic resource] :$$bmodeling and optimization with case studies /$$cGiorgio Fasano, János D. Pintér, editors. 000771384 260__ $$aSwitzerland :$$bSpringer,$$c2016. 000771384 300__ $$a1 online resource. 000771384 336__ $$atext$$btxt$$2rdacontent 000771384 337__ $$acomputer$$bc$$2rdamedia 000771384 338__ $$aonline resource$$bcr$$2rdacarrier 000771384 4901_ $$aSpringer optimization and its applications,$$x1931-6828 ;$$vvolume 114 000771384 500__ $$aIncludes index. 000771384 5050_ $$aPreface; Acknowledgments; MSC 2010 Classification: Suggested Categories and Keywords for the Book; Contents; Editors; Advanced Space Vehicle Design Taking into Account Multidisciplinary Couplings and Mixed Epistemic/Aleatory Uncertainties ; Nomenclature; 1 Introduction; 2 MDO Decomposition Strategy for Launch Vehicle Design; 2.1 General MDO Formulation and Review of Main MDO Approaches; 2.2 Stage-Wise decomposition for Optimal Rocket Design; 2.2.1 Theoretical Formulations; 2.2.2 Application of SWORD to Launch Vehicle Design; 3 Introduction of Uncertainty in the Design Process 000771384 5058_ $$a3.1 Optimization of Design Rules and Safety Margins Taking into Account Mixed Epistemic/Aleatory Uncertainties3.2 Uncertainty Multidisciplinary Design Optimization; 3.2.1 Theoretical Approach for Interdisciplinary Coupling Satisfaction in the Presence of Uncertainty; 3.2.2 Application for Launch Vehicle Design; 4 Conclusion; References; Using Direct Transcription to Compute Optimal Low Thrust Transfers Between Libration Point Orbits; 1 The Optimal Control Problem; 2 Transcription Method; 3 Runge-Kutta Methods; 3.1 Lobatto IIIA, S = 2; 3.2 Lobatto IIIA, S = 3; 3.3 Lobatto IIIA, S = 4 000771384 5058_ $$a3.4 Lobatto IIIA, S = 54 Nonlinear Programming; 5 Mesh Refinement; 6 Optimal Low Thrust Transfers Between Libration Point Orbits; 6.1 Introduction; 6.2 Dynamic Model; 6.3 Lyapunov Orbits; 6.4 Adjoint Equations; 7 Numerical Results; 7.1 Short Transfer; 7.2 Long Transfer; 8 Computational Comparisons; 8.1 Spline Approximation; 8.2 Mesh Refinement Strategy; 8.3 Indirect Collocation; 9 Summary; Appendix: Lobatto IIIA Method Coefficients; References; Tentative Solutions for Indirect Optimization of SpacecraftTrajectories; 1 Introduction; 2 Optimal Control Problem 000771384 5058_ $$a3 Application to Space Trajectories Optimization4 BVP Solution and Improvements of Numerical Accuracy; 4.1 Gradient Evaluation; 4.2 Thrust Discontinuities; 4.3 Multiple Shooting; 5 Techniques to Improve Convergence; 6 Final Remarks; References; Resource-Constrained Scheduling with Non-constant Capacity and Non-regular Activities; 1 Introduction; 2 Time-Indexed Formulation; 3 Applications and Computational Results; 3.1 Basic Test Set; 3.2 Test Sets A, B, C, D, E and F; 3.3 Test Set G; 3.4 Tests Extracted from Fekete's and Shepers' Set; 4 Conclusions; Appendix; Test Set F Power Consumption 000771384 5058_ $$aTest set B Power FunctionTest Set C Power Function; Test Set D Power Function; Test Set E Power Function; Test set F Power Function; Test Set G: Resource 1 Function; Test Set G: Resource 2 Function; Test Set G: Resource 3 Function; References; Packing Problems in Space Solved by CPLEX: An Experimental Analysis; 1 Introduction; 2 MILP Model and Heuristic Approach; 3 Experimental Framework and Results; 4 Conclusive Remarks; Appendix; References; Designing Complex Interplanetary Trajectories for the Global Trajectory Optimization Competitions; 1 Introduction; 2 Building Blocks 000771384 506__ $$aAccess limited to authorized users. 000771384 650_0 $$aAstronautics. 000771384 650_0 $$aAeronautics. 000771384 7001_ $$aFasano, Giorgio,$$eeditor. 000771384 7001_ $$aPintér, János D.$$eeditor. 000771384 77608 $$iPrint version:$$z3319415069$$z9783319415062$$w(OCoLC)951642892 000771384 830_0 $$aSpringer optimization and its applications ;$$vv. 114. 000771384 852__ $$bebk 000771384 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-319-41508-6$$zOnline Access$$91397441.1 000771384 909CO $$ooai:library.usi.edu:771384$$pGLOBAL_SET 000771384 980__ $$aEBOOK 000771384 980__ $$aBIB 000771384 982__ $$aEbook 000771384 983__ $$aOnline 000771384 994__ $$a92$$bISE