Pseudospectral Convex Optimization for Powered Descent and Landing
暂无分享,去创建一个
[1] Stephen P. Boyd,et al. Applications of second-order cone programming , 1998 .
[2] F. Bennett. Lunar descent and ascent trajectories , 1970 .
[3] Jos F. Sturm,et al. A Matlab toolbox for optimization over symmetric cones , 1999 .
[4] Alexander Domahidi. Methods and tools for embedded optimization and control , 2013 .
[5] Michael A. Saunders,et al. User's Guide for SNOPT Version 7.4: Software for Large-Scale Nonlinear Programming , 2015 .
[6] Stephen P. Boyd,et al. ECOS: An SOCP solver for embedded systems , 2013, 2013 European Control Conference (ECC).
[7] Ronald R. Sostaric,et al. Powered Descent Guidance Methods For The Moon and Mars , 2005 .
[8] Marco Sagliano,et al. Performance analysis of linear and nonlinear techniques for automatic scaling of discretized control problems , 2014, Oper. Res. Lett..
[9] P. Lu,et al. Entry Trajectory Optimization by Second-Order Cone Programming , 2016 .
[10] Wei Kang,et al. Pseudospectral Feedback Control: Foundations, Examples and Experimental Results , 2006 .
[11] Irene A. Stegun,et al. Handbook of Mathematical Functions. , 1966 .
[12] Marco Sagliano,et al. Exact Hybrid Jacobian Computation for OptimalTrajectory Generation via Dual Number Theory , 2016 .
[13] Arkadi Nemirovski,et al. Lectures on modern convex optimization - analysis, algorithms, and engineering applications , 2001, MPS-SIAM series on optimization.
[14] Qi Gong,et al. Connections between the covector mapping theorem and convergence of pseudospectral methods for optimal control , 2008, Comput. Optim. Appl..
[15] Ping Lu,et al. Solving Nonconvex Optimal Control Problems by Convex Optimization , 2014 .
[16] Marco Sagliano,et al. SPARTAN: An Improved Global Pseudospectral Algorithm for High-Fidelity Entry-Descent-Landing Guidance Analysis , 2015 .
[17] Marco Sagliano,et al. SPARTAN: A Novel Pseudospectral Algorithm for Entry, Descent, and Landing Analysis , 2018 .
[18] Marco Sagliano,et al. On the Radau pseudospectral method: theoretical and implementation advances , 2017, CEAS Space Journal.
[19] Robert N. Ingoldby. Guidance and Control System Design of the Viking Planetary Lander , 1977 .
[20] Kim-Chuan Toh,et al. On the Implementation and Usage of SDPT3 – A Matlab Software Package for Semidefinite-Quadratic-Linear Programming, Version 4.0 , 2012 .
[21] S. Ploen,et al. A Powered Descent Guidance Algorithm for Mars Pinpoint Landing , 2005 .
[22] Lorenz T. Biegler,et al. On the implementation of an interior-point filter line-search algorithm for large-scale nonlinear programming , 2006, Math. Program..
[23] Colin R. McInnes. Gravity-turn descent from low circular orbit conditions , 2003 .
[24] Marco Sagliano,et al. Development of a Novel Algorithm for High Performance Reentry Guidance , 2016 .
[25] Joaquim R. R. A. Martins,et al. The complex-step derivative approximation , 2003, TOMS.
[26] Marco Sagliano,et al. Hybrid Jacobian Computation for Fast Optimal Trajectories Generation , 2013 .
[27] Behçet Açikmese,et al. Lossless Convexification of Nonconvex Control Bound and Pointing Constraints of the Soft Landing Optimal Control Problem , 2013, IEEE Transactions on Control Systems Technology.
[28] Michael Szmuk,et al. Successive Convexification for Mars 6-DoF Powered Descent Landing Guidance , 2017 .
[29] Stephen P. Boyd,et al. CVXGEN: a code generator for embedded convex optimization , 2011, Optimization and Engineering.
[30] Joel Benito,et al. Implementation and Experimental Demonstration of Onboard Powered-Descent Guidance , 2017 .
[31] I. Michael Ross,et al. Direct trajectory optimization by a Chebyshev pseudospectral method , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).
[32] Chee Wei Tan,et al. Introduction to Convex Optimization , 2010 .
[33] Frederick Serricchio,et al. In-flight experience of the Mars Science Laboratory Guidance, Navigation, and Control system for Entry, Descent, and Landing , 2015 .
[34] Behcet Acikmese,et al. Minimum-Landing-Error Powered-Descent Guidance for Mars Landing Using Convex Optimization , 2010 .
[35] Andrew E. Johnson,et al. Flight testing of trajectories computed by G-FOLD: Fuel optimal large divert guidance algorithm for planetary landing , 2013 .
[36] Daniel Dueri,et al. Customized Real-Time Interior-Point Methods for Onboard Powered-Descent Guidance , 2017 .
[37] M. A. Connor,et al. Gravity turn trajectories through the atmosphere. , 1966 .
[38] J. Jungmann. Gravity turn trajectories through planetary atmospheres , 1967 .
[39] Divya Garg,et al. ADVANCES IN GLOBAL PSEUDOSPECTRAL METHODS FOR OPTIMAL CONTROL , 2011 .
[40] Behcet Acikmese,et al. Convex programming approach to powered descent guidance for mars landing , 2007 .