-
-
Mission Feasibility Analysis on Deflecting Earth-Crossing Objects using a Power Limited Laser Ablating Spacecraft
-
Hardware-in-the-Loop Simulations of GPS-Based Navigation and Control for Satellite Formation Flying
-
Satellite Orbit Determination Using a Batch Filter Based on the Unscented Transformation
-
Nonlinear attitude control of a tether-connected multi-satellite in three-dimensional space
-
Spacecraft formation flying for Earth-crossing object deflections using a power limited laser ablating
-
A lunar cargo mission design strategy using variable low thrust
-
Investigating suitable orbits for the Swarm constellation mission ? The frozen orbit
-
Hybrid Optimization for Multiple-Impulse Reconfiguration Trajectories of Satellite Formation Flying
-
Analytic Solution for Fuel-Optimal Reconfiguration in Relative Motion
-
Decentralized Coordinated Attitude Control for Satellite Formation Flying via the State-Dependent Riccati Equation Technique
-
Orbit Determination Using the Geomagnetic Field Measurement via the Unscented Kalman Filter
-
Global Solution for the Optimal Feedback Control of the Underactuated Heisenberg System
-
Determination of Optimal Feedback Terminal Controllers for General Boundary Conditions using Generating Functions
-
Mission Design for Human Outer Planet Exploration (HOPE) using a Magnetoplasma Spacecraft
-
Solving Optimal Continuous Thrust Rendezvous Problems with Generating Functions
-
Optimal Low-Thrust Intercept/Rendezvous Trajectories to Earth-Crossing Objects
-
Fuel-Optimal Transfers Between Coplanar Circular Orbits Using Variable Specific-Impulse Engines
-
Planar High-Thrust and Low-Thrust Orbital Transfers from earth to Europa
-
Deflection of Earth-Crossing Asteroids/Comets using Rendezvous Spacecraft and Laser Ablation
