In this paper, a novel covariance tracking receding horizon (CTRH) process is proposed to
design a robust control algorithm. Some drawbacks of the equivalent robust algorithms …

The gradual expansion of infrastructure on and around the Moon is key to establishing the
long-term exploration of the Moon through eg, NASA's Artemis and Commercial Lunar …

This paper presents a new approach to optimal trajectory design that considers uncertainties
in the system, referred to herein as robust trajectory optimization. This approach assumes an …

Entry guidance is a fundamental element of atmospheric entry missions. However, during
the atmospheric entry, there are many uncertainties that cannot be predicted and ultimately …

A new approach to optimal trajectory design is the determination of optimal trajectories that
are robust to initial trajectory dispersions, navigation errors, maneuver execution errors, and …

Path planning in an uncertain environment is a key enabler of true vehicle autonomy. Over
the past two decades, numerous approaches have been developed to account for errors in …

For atmospheric entry vehicles, guidance design can be accomplished by solving an optimal
issue using optimal control theories. However, traditional design methods generally focus on …

A robust trajectory planning method for non-cooperative target rendezvous is investigated
based on closed-loop uncertainty analysis. The proposed method addresses the issue that …

One possibility for satellite cluster flight is to control relative distances using differential drag.
The idea is to increase or decrease the drag acceleration on each satellite by changing its …

A time-varying output covariance assignment problem in the presence of a stochastic
disturbance is solved using finite-horizon optimal control formulation. It is shown that an …