Convex optimization for trajectory generation: A tutorial on generating dynamically feasible trajectories reliably and efficiently

D Malyuta, TP Reynolds, M Szmuk… - IEEE Control …, 2022 - ieeexplore.ieee.org
Reliable and efficient trajectory generation methods are a fundamental need for
autonomous dynamical systems. The goal of this article is to provide a comprehensive …

Advances in trajectory optimization for space vehicle control

D Malyuta, Y Yu, P Elango, B Açıkmeşe - Annual Reviews in Control, 2021 - Elsevier
Abstract Space mission design places a premium on cost and operational efficiency. The
search for new science and life beyond Earth calls for spacecraft that can deliver scientific …

Convex optimization for trajectory generation

D Malyuta, TP Reynolds, M Szmuk, T Lew… - arXiv preprint arXiv …, 2021 - arxiv.org
Reliable and efficient trajectory generation methods are a fundamental need for
autonomous dynamical systems of tomorrow. The goal of this article is to provide a …

Convex optimization-based trajectory planning for quadrotors landing on aerial vehicle carriers

Z Shen, G Zhou, H Huang, C Huang… - IEEE Transactions …, 2023 - ieeexplore.ieee.org
This paper presents a novel trajectory planning algorithm for quadrotors landing on aerial
vehicle carriers (AVCs). The algorithm involves a quadrotor trajectory planning method …

Customized real-time first-order methods for onboard dual quaternion-based 6-DoF powered-descent guidance

AG Kamath, P Elango, T Kim, S Mceowen… - AIAA SciTech 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-2003. vid The dual quaternion-
based 6-DoF powered-descent guidance algorithm (DQG) was selected as the candidate …

Trajectory optimization for spacecraft autonomous rendezvous and docking with compound state-triggered constraints

Y Zhang, B Zhu, M Cheng, S Li - Aerospace Science and Technology, 2022 - Elsevier
In this paper, a guidance algorithm is presented based on successive convexification for the
generation of fuel-optimal 6-DOF spacecraft close proximity trajectory subject to multiple …

A real-time algorithm for non-convex powered descent guidance

T Reynolds, D Malyuta, M Mesbahi… - AIAA Scitech 2020 …, 2020 - arc.aiaa.org
The on-board solution of constrained optimal control problems is a key technology for future
entry, descent and landing systems. The constraints that must be satisfied to enable …

A survey on convex optimization for guidance and control of vehicular systems

Z Wang - Annual Reviews in Control, 2024 - Elsevier
Guidance and control (G&C) technologies play a central role in the development and
operation of vehicular systems. The emergence of computational guidance and control …

Fast trajectory optimization via successive convexification for spacecraft rendezvous with integer constraints

D Malyuta, T Reynolds, M Szmuk, B Acikmese… - AIAA Scitech 2020 …, 2020 - arc.aiaa.org
In this paper we present a fast method based on successive convexification for generating
fuel-optimized spacecraft rendezvous trajectories in the presence of mixed-integer …

A joint guidance and control framework for autonomous obstacle avoidance in quadrotor formations under model uncertainty

Z Ma, Q Wang, H Chen - Aerospace Science and Technology, 2023 - Elsevier
This paper presents a novel joint guidance and control framework for autonomous obstacle
avoidance and swift maneuvering of quadrotor formations under model uncertainty. In this …