Air-breathing hypersonic vehicle has great military and potential economic value due to its
characteristics: high velocity, long range, quick response. Therefore, the development of …

Future Mars landing missions will require the capability of precise landing at certain sites for
specific scientific interests to gather more valuable scientific information. Autonomous …

Based on the relative motion dynamic model illustrated by CW equations, the problem of
robust Hinfin control for a class of spacecraft rendezvous systems is investigated, which …

This paper studies a novel guidance framework of the vehicle against a high-speed and
maneuvering target based on deep reinforcement learning (DRL) considering the energy …

The terminal guidance problem for missiles intercepting maneuvering targets with terminal
impact angle constraints is investigated. Regarding the target acceleration as an unknown …

The performance of the zero-effort-miss/zero-effort-velocity feedback guidance algorithm is
evaluated through practical space application examples. The zero-effort-miss/zero-effort …

The sizing and capability definitions of reusable launchers during high-speed recovery are
very challenging problems. In this paper, a convex optimization guidance algorithm for this …

As small celestial body exploration advances, higher requirements with regard to system
safety and landing precision are proposed for future landing and sample return missions …

This paper studies the mechanics of reusable retropropelled flight of slender low lift-to-drag
bodies via integrated guidance and control simulations. To do this, a simulation benchmark …

This paper summarizes the autonomous guidance methods (AGMs) for pinpoint soft landing
on celestial surfaces. We first review the development of powered descent guidance …