Linked e-resources
Details
Table of Contents
Advances in the Control Propellant Minimization for the Next Generation Gravity Mission (A. Anselmi )
Transition of Two-dimensional Quasi-periodic Invariant Tori in the Real-ephemeris Model of the Earth-Moon System (N. Baresi)
Hypersonic Point-to-Point Travel for the Common Man (E. Mooij)
Bifocal Metrology Applications in Space Engineering (F. Bresciani)
A Revisited Analysis of the Radioisotope Sail and its Possible Application to Relativistic Spaceflight (L. Derosa)
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats (G. Di Domenico)
Data Reduction for Optimizing the Attitude Control Dispatch in a Spacecraft (C. Durand)
Second Order Sufcient Conditions of Strong Minimality with applications to Orbital Transfers (L. Mazzini)
Evolutionary Optimisation of a Flexible-Launcher Simple Adaptive Control System (E. Mooij)
Optimization and Solution Approaches in Utilizing Wireless Sensor Networks for Exploring Moon Planets and Space (O. Ozkan)
Near-Optimal Guidance and Pulse-Modulated Reduced Attitude Control for Orbit Injection (M. Pontani)
A Pareto front numerical reconstruction strategy applied to a satellite system conceptual design (M. Sebastin)
Indirect optimization of robust orbit transfer considering thruster underperformance (F. Simeoni)
Time-Varying Lyapunov Control Laws with Enhanced Estimation of Distribution Algorithm for Low-Thrust Trajectory Design (R. Armellin).
Transition of Two-dimensional Quasi-periodic Invariant Tori in the Real-ephemeris Model of the Earth-Moon System (N. Baresi)
Hypersonic Point-to-Point Travel for the Common Man (E. Mooij)
Bifocal Metrology Applications in Space Engineering (F. Bresciani)
A Revisited Analysis of the Radioisotope Sail and its Possible Application to Relativistic Spaceflight (L. Derosa)
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats (G. Di Domenico)
Data Reduction for Optimizing the Attitude Control Dispatch in a Spacecraft (C. Durand)
Second Order Sufcient Conditions of Strong Minimality with applications to Orbital Transfers (L. Mazzini)
Evolutionary Optimisation of a Flexible-Launcher Simple Adaptive Control System (E. Mooij)
Optimization and Solution Approaches in Utilizing Wireless Sensor Networks for Exploring Moon Planets and Space (O. Ozkan)
Near-Optimal Guidance and Pulse-Modulated Reduced Attitude Control for Orbit Injection (M. Pontani)
A Pareto front numerical reconstruction strategy applied to a satellite system conceptual design (M. Sebastin)
Indirect optimization of robust orbit transfer considering thruster underperformance (F. Simeoni)
Time-Varying Lyapunov Control Laws with Enhanced Estimation of Distribution Algorithm for Low-Thrust Trajectory Design (R. Armellin).