Ascent trajectory optimization for air‐breathing vehicles in consideration of launch window

[1]  Huiqiang Zhang,et al.  Feasibility Study of a DRBCC-Powered Single-Stage-To-Orbit Launch Vehicle , 2016 .

[2]  Lei Liu,et al.  Ascent trajectory optimization of hypersonic vehicle based on improved Particle Swarm algorithm , 2015, 2015 Chinese Automation Congress (CAC).

[3]  S. W. Paris,et al.  Application of an advanced trajectory optimization method to ramjet propelled missiles , 1980 .

[4]  Li Zhou,et al.  Dynamic surface control based on neural network for an air-breathing hypersonic vehicle , 2015 .

[5]  T. Williams,et al.  Launch Window Analysis for the Magnetospheric Multiscale Mission , 2012 .

[6]  Hongyu Zhou,et al.  Ascent phase trajectory optimization for vehicle with multi-combined cycle engine based on improved particle swarm optimization , 2017 .

[7]  Ping Lu,et al.  Fast Ascent Trajectory Optimization for Hypersonic Air-Breathing Vehicles , 2010 .

[8]  Hexi Baoyin,et al.  Lunar exploration phase III: Launch window and trajectory design for a lunar lander , 2015 .

[9]  Zhengtao Ding,et al.  Modeling and nonlinear control for air-breathing hypersonic vehicle with variable geometry inlet , 2017 .

[10]  Dean Eppler,et al.  Comparing Apollo and Mars Exploration Rover (MER)/phoenix operations paradigms for human exploration during NASA Desert-RATS science operations , 2013 .

[11]  Kenneth D. Mease,et al.  Aerospace plane guidance using time-scale decomposition and feedback linearization , 1992 .

[12]  Guoqiang He,et al.  Analysis and reduction of skin-friction in a rocket-based combined-cycle engine flow path operating from Mach 1.5 to 6.0 , 2018, Acta Astronautica.

[13]  R. Boukenoui,et al.  A new Golden Section method-based maximum power point tracking algorithm for photovoltaic systems , 2016 .

[14]  V. Azhmyakov,et al.  A modified pseudospectral method for solving trajectory optimization problems with singular arc , 2017 .

[15]  Dario Giuseppe Pastrone,et al.  Multi-Objective Optimization of Rocket-Based Combined-Cycle Engine Performance Using a Hybrid Evolutionary Algorithm , 2009 .

[16]  Rui Xue,et al.  Combustion oscillation study in a kerosene fueled rocket-based combined-cycle engine combustor , 2016 .

[17]  F. Johnson Free return circumlunar trajectories from launch windows with fixed launch azimuths. , 1963 .

[18]  Huijun Gao,et al.  Reference output tracking control for a flexible air-breathing hypersonic vehicle via output feedback , 2012 .

[19]  Roger Shawyer,et al.  Second generation EmDrive propulsion applied to SSTO launcher and interstellar probe , 2015 .

[20]  Hongyu Zhou,et al.  Reentry guidance with constrained impact for hypersonic weapon by novel particle swarm optimization , 2018, Aerospace Science and Technology.

[21]  Yuan Wang,et al.  Overview of the key technologies of combined cycle engine precooling systems and the advanced applications of micro-channel heat transfer , 2014 .

[22]  Guillermo Paniagua,et al.  Numerical Model of a Variable-Combined-Cycle Engine for Dual Subsonic and Supersonic Cruise , 2013 .

[23]  I. Michael Ross,et al.  Optimal Nonlinear Feedback Guidance for Reentry Vehicles , 2006 .

[24]  Ping Lu,et al.  Closed-loop endoatmospheric ascent guidance , 2003 .

[25]  Trevor Moeller,et al.  Assessment of Aerospike Nozzle for Single-Stage to Orbit Flight , 2015 .

[26]  Masataka Nishi Towards bounded model checking using nonlinear programming solver , 2016, 2016 31st IEEE/ACM International Conference on Automated Software Engineering (ASE).

[27]  Ju-Jang Lee,et al.  Trajectory Optimization With Particle Swarm Optimization for Manipulator Motion Planning , 2015, IEEE Transactions on Industrial Informatics.

[28]  Hexi Baoyin,et al.  Generation of launch windows for high-accuracy lunar trajectories , 2015 .

[29]  Howard D. Curtis Chapter 4 – Orbits in Three Dimensions , 2010 .

[30]  Daren Yu,et al.  Trajectory optimization for a ramjet-powered vehicle in ascent phase via the Gauss pseudospectral method , 2017 .

[31]  Anthony J. Calise,et al.  Trajectory optimization and guidance law development for transatmospheric vehicles , 1989, Proceedings. ICCON IEEE International Conference on Control and Applications.

[32]  Martin Hechler Launch windows for libration point missions , 2009 .

[33]  T. Inanc,et al.  A multiphase DMOC‐based trajectory optimization method , 2018 .

[34]  David K. Schmidt Optimum Mission Performance and Multivariable Flight Guidance for Airbreathing Launch Vehicles , 1997 .

[35]  Kiichi Urahama,et al.  Gradient Projection Network: Analog Solver for Linearly Constrained Nonlinear Programming , 1996, Neural Computation.