Static Attitude Determination Methods
Review of Control and Estimation Theory
Filtering for Attitude Estimation and Calibration
Attitude Kinematics and Dynamics
Matrices, Vectors, Frames, Transforms
Correction to: Fundamentals of Spacecraft Attitude Determination and Control
Machine Learning and Evolutionary Techniques in Interplanetary Trajectory Design
A Catalogue of Parametric Time-Optimal Transfers for All-Electric GEO Satellites
Data Reduction for Optimizing the Attitude Control Dispatch in a Spacecraft
Ascent Trajectory Optimization and Neighboring Optimal Guidance of Multistage Launch Vehicles
Real-Time Optimal Control Using TransWORHP and WORHP Zen
Global Optimization of Continuous-Thrust Trajectories Using Evolutionary Neurocontrol
Theory and Applications of Optimal Finite Thrust Orbital Transfers
Control Propellant Minimization for the Next Generation Gravity Mission
Optimization Issues in the Problem of Small Satellite Attitude Determination and Control
Single-Stage-to-Orbit Space-Plane Trajectory Performance Analysis
Optimal Topological Design of a Thermal Isolator for a Monopropellant Space Thruster
Dynamic System Control Dispatch: A Global Optimization Approach
Indirect Optimization of Robust Orbit Transfer Considering Thruster Underperformance
Second-order Sufficient Conditions of Strong Minimality with applications to Orbital Transfers
Optimized Packings in Space Engineering Applications: Part I
Choice of the Optimal Launch Date for Interplanetary Missions
Hypersonic Point-to-Point Travel for the Common Man
Evolutionary Optimisation of a Flexible-Launcher Simple Adaptive Control System
Near-Optimal Guidance and Pulse-Modulated Reduced-Attitude Control for Orbit Injection
Optimized Packings in Space Engineering Applications: Part II
A Pareto Front Numerical Reconstruction Strategy Applied to a Satellite System Conceptual Design
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats
Bifocal Metrology Applications in Space Engineering
Advances in the Control Propellant Minimization for the Next Generation Gravity Mission