All Stories

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