All Stories

  1. Multifidelity HDMR Surrogates for Thermal Protection System Heat Flux Hybrid Uncertainty Quantification
  2. Stochastic Bayesian Model Updating to Reduce Epistemic Uncertainty in Satellite Attitude Propagation
  3. Hyperspectral Lightcurve Inversion for Attitude Determination
  4. Modelling Future Launch Traffic and its Effect on the LEO Operational Environment
  5. Vision-based Synchronised Control of Space Manipulator’s Dynamic Motion and Spacecraft’ Attitude
  6. Angles-Only Navigation in the Proximity of a Binary Asteroid System
  7. Robust Trajectory Optimisation of a TSTO Spaceplane Using Uncertainty-Based Atmospheric Models
  8. Structured-chromosome GA optimisation for satellite tracking
  9. Solving multi-objective dynamic travelling salesman problems by relaxation
  10. Direct Transcription of Optimal Control Problems with Finite Elements on Bernstein Basis
  11. Direct Solution of Multi-Objective Optimal Control Problems Applied to Spaceplane Mission Design
  12. Study of Lorentz Force on Debris with High Area-to-Mass Ratios
  13. Angles-Only Navigation of a Formation in the Proximity of a Binary System
  14. Multi-Objective Optimal Control of Re-entry and Abort Scenarios
  15. Post-launch analysis of the deployment dynamics of a space web sounding rocket experiment
  16. Analysis of the de-orbiting and re-entry of space objects with high area to mass ratio
  17. Multi-Objective Optimal Control of the Ascent Trajectories of Launch Vehicles
  18. Low-thrust tour of the main belt asteroids
  19. Multi-objective optimisation of constellation deployment using low-thrust propulsion
  20. Multi Agent Collaborative Search
  21. Simulation and Control of a Space Web Deployed by Centrifugal Forces in a Sounding Rocket Experiment
  22. Nuclear cycler: An incremental approach to the deflection of asteroids
  23. Asteroid rotation and orbit control via laser ablation
  24. Autonomous navigation of a spacecraft formation in the proximity of an asteroid
  25. Preface: Advances in asteroid and space debris science and technology – Part 2
  26. Mission and system design for the manipulation of PHOs with space-borne lasers
  27. Optimal control of a space-borne laser system for a 100 m asteroid deflection under uncertainties
  28. Control analysis for a contactless de-tumbling method based on eddy currents: problem definition and approximate proposed solutions
  29. Asteroid and Space Debris Manipulation: Advances from the Stardust Research Network
  30. Sun-Earth L1 and L2 to Moon Transfers Exploiting Natural Dynamics
  31. Incremental planning of multi-gravity assist trajectories
  32. Deflection of uncooperative targets using laser ablation
  33. Preface: Advances in Asteroid and Space Debris Science and Technology – Part 1
  34. Sensitivity Analysis towards Probabilistic Re-Entry Modeling of Spacecraft and Space Debris
  35. End-of-life disposal concepts for Libration Point Orbit and Highly Elliptical Orbit missions
  36. Multi-population inflationary differential evolution algorithm with Adaptive Local Restart
  37. Detumbling large space debris via laser ablation
  38. A Novel Multiobjective Evolutionary Algorithm Based on Regression Analysis
  39. Extended analytical formulas for the perturbed Keplerian motion under a constant control acceleration
  40. Inflatable shape changing colonies assembling versatile smart space structures
  41. (Non) convergence results for the differential evolution method
  42. Improved laser ablation model for asteroid deflection
  43. Sun–Earth $$L_{1}$$ L 1 and $$L_{2}$$ L 2 to Moon transfers exploiting natural dynamics
  44. Recent advances in laser ablation modelling for asteroid deflection methods
  45. Adaptive Inflationary Differential Evolution
  46. A multidirectional Physarum solver for the automated design of space trajectories
  47. An evolutionary approach to the solution of multi-objective min-max problems in evidence-based robust optimization
  48. Multibody Dynamics for Biologically Inspired Smart Space Structure
  49. Computational Intelligence in Aerospace Sciences
  50. Computational Intelligence in Aerospace Sciences
  51. Multidisciplinary Design Optimization of Aerospace Transportation Systems
  52. On the Global Optimization of Multigravity Assist Trajectories with Evolutionary Algorithms
  53. Multidirectional Incremental Space Trajectory Planning
  54. Mission and System Design
  55. Contingency and recovery options for the European Student Moon Orbiter
  56. An Incremental Algorithm for the Optimization of Multiple Gravity Assist Trajectories
  57. Heuristic Scheduling Algorithm Oriented Dynamic Tasks for Imaging Satellites
  58. Experimental analysis of laser ablated plumes for asteroid deflection and exploitation
  59. Deflecting Small Asteroids using Laser Ablation: Deep Space Navigation and Asteroid Orbit Control for LightTouch 2 Mission
  60. Robust Design of a Reentry Unmanned Space Vehicle by Multifidelity Evolution Control
  61. Computational methods in engineering design and optimization
  62. Surrogate-based Maximisation of Belief Function for Robust Design Optimisation
  63. Multi Agent Collaborative Search based on Tchebycheff decomposition
  64. Time-optimal trajectories to circumsolar space using solar electric propulsion
  65. Orbit determination and control for the European Student Moon Orbiter
  66. Design of a formation of solar pumped lasers for asteroid deflection
  67. Potential of laser-induced ablation for future space applications
  68. SPS-ALPHA: The First Practical Solar Power Satellite via Arbitrarily Large Phased Array (A 2011-2012 NIAC Project)
  69. Evidence-based robust design of deflection actions for near Earth objects
  70. Robust Aerodynamic Design of Variable Speed Wind Turbine Rotors
  71. Direct transcription of low-thrust trajectories with finite trajectory elements
  72. Preliminary Design of Debris Removal Missions by Means of Simplified Models for Low-Thrust, Many-Revolution Transfers
  73. Low-Thrust-Enabled Highly-Non-Keplerian Orbits in Support of Future Mars Exploration
  74. An Inflationary Differential Evolution Algorithm for Space Trajectory Optimization
  75. Computing the Set of Epsilon-Efficient Solutions in Multiobjective Space Mission Design
  76. Robust design of a re-entry unmanned space vehicle by multi-fidelity evolution control
  77. MGA trajectory planning with an ACO-inspired algorithm
  78. Extension of the Sun-Synchronous Orbit
  79. Automated Multigravity Assist Trajectory Planning with a Modified Ant Colony Algorithm
  80. Multidisciplinary Design of a Micro-USV for Reentry Operations
  81. Finite Elements in Time: A Direct Transcription Method for Optimal Control Problems
  82. A Novel Interplanetary Communications Relay
  83. An Ant System algorithm for automated trajectory planning
  84. A hybrid multiobjective optimization algorithm applied to space trajectory optimization
  85. Computing approximate solutions of scalar optimization problems and applications in space mission design
  86. On the deflection of asteroids with mirrors
  87. Analysis of Some Global Optimization Algorithms for Space Trajectory Design
  88. Preliminary space mission design under uncertainty
  89. Robust Preliminary Space Mission Design under Uncertainty
  90. A multi-mirror solution for the deflection of dangerous NEOS
  91. Optimal low-thrust trajectories to asteroids through an algorithm based on differential dynamic programming
  92. Semi-Analytical Solution for the Optimal Low-Thrust Deflection of Near-Earth Objects
  93. Evolutionary Neurocontrol: A Novel Method for Low-Thrust Gravity-Assist Trajectory Optimization
  94. Designing optimal low-thrust gravity-assist trajectories using space pruning and a multi-objective approach
  95. Approach to Model Interest for a Planetary Rover through Dezert-Smarandache Theory
  96. Memetic Strategies for Global Trajectory Optimisation
  97. Multicriteria Comparison Among Several Mitigation Strategies for Dangerous Near-Earth Objects
  98. On Testing Global Optimization Algorithms for Space Trajectory Design
  99. Mirror Formation Control in the Vicinity of an Asteroid
  100. A hybrid multiagent approach for global trajectory optimization
  101. Optimal Impact Strategies for Asteroid Deflection
  102. Design of optimal spacecraft‐asteroid formations through a hybrid global optimization approach
  103. Approximate Solutions in Space Mission Design
  104. On the design of low-thrust transfers throughL1for the ESMO mission
  105. A behavioral-based meta-heuristic for robust global trajectory optimization
  106. Optimal design for a NEO tracking spacecraft formation
  107. A Multi-criteria Assessment of Deflection Methods for Dangerous NEOs
  108. Comparison of Single and Multi-Spacecraft Configurations for NEA Deflection by Solar Sublimation
  109. A Non-Deterministic Planner for Planetary Rover Autonomy
  110. Autonomous Rover Control with Behavioral Algorithms and Neural Networks
  111. Design of Earth–Mars transfer trajectories using evolutionary-branching technique
  112. A Systematic-Heuristic Approach for Space Trajectory Design
  113. Design of Low-Thrust Trajectories for the Exploration of the Outer Solar System
  114. Design of Earth-Mars Transfer Trajectories Using Evolution-Branching Technique
  115. Trajectory Design Combining Low-Thrust and Gravity Assist Manoeuvres
  116. Combining Evolution Programs and Gradient Methods for WSB Transfer Optimisation
  117. Robust Optimisation of Trajectories Intercepting Dangerous NEO
  118. Deep Space Autonomous Orbit Determination Using CCD
  119. Autonomous navigation of a rover for planetary exploration
  120. Hybrid Behavioral-Based Multiobjective Space Trajectory Optimization
  121. Incremental Techniques for Global Space Trajectory Design