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Model Predictive Control (MPC) is widely adopted for agile multirotor vehicles, yet achieving both stability and obstacle-free flight is particularly challenging when a payload is suspended beneath the airframe. This paper introduces a…

机器人学 · 计算机科学 2026-03-11 Seyedreza Rezaei , Junjie Kang , Amaldev Haridevan , Jinjun Shan

We propose a robust nonlinear model predictive control (MPC) scheme for trajectory-tracking control of autonomous vehicles at the limits of handling on non-planar road surfaces. We derive the dynamics from first principles and selectively…

系统与控制 · 电气工程与系统科学 2026-04-22 Joscha F. Bongard , Georg Jank , Simon Sagmeister , Boris Lohmann

Given the cost and critical functions of satellite constellations, ensuring mission longevity and safe decommissioning is essential for space sustainability. This article presents a Model Predictive Control for spacecraft trajectory and…

机器人学 · 计算机科学 2025-09-03 Raphael Stöckner , Pedro Roque , Maria Charitidou , Dimos V. Dimarogonas

Designing a model predictive control (MPC) scheme that enables a mobile robot to safely navigate through an obstacle-filled environment is a complicated yet essential task in robotics. In this technical report, safety refers to ensuring…

机器人学 · 计算机科学 2025-08-12 Dennis Benders , Laura Ferranti , Johannes Köhler

In this paper, a control scheme is developed based on an input constrained Model Predictive Controller (MPC) and the idea of modifying the reference command to enforce constraints, usual of Reference Governors (RG). The proposed scheme,…

系统与控制 · 电气工程与系统科学 2022-10-21 Miguel Castroviejo Fernandez , Jordan Leung , Ilya Kolmanovsky

In this paper, a sampling-based Stochastic Model Predictive Control algorithm is proposed for discrete-time linear systems subject to both parametric uncertainties and additive disturbances. One of the main drivers for the development of…

Among various satellite actuators, magnetic torquers have been widely equipped for stabilization and attitude control of small satellites. Although magnetorquers are generally used with other actuators, such as momentum wheels, this paper…

系统与控制 · 电气工程与系统科学 2024-01-23 Kota Kondo , Yasuhiro Yoshimura , Shiji Nagasaki , Toshiya Hanada

This paper presents a navigation strategy to fly to the Moon along a Weak Stability Boundary transfer trajectory. A particular strategy is devised to ensure capture into an uncontrolled relatively stable orbit at the Moon. Both uncertainty…

最优化与控制 · 数学 2015-06-05 Massimo Vetrisano , Willem van der Weg , Massimiliano Vasile

This paper investigates the infinite horizon optimal control problem (OCP) for space applications characterized by nonlinear dynamics. The proposed approach divides the problem into a finite horizon OCP with a regularized terminal cost,…

最优化与控制 · 数学 2025-10-13 Abhijeet , Mohamed Naveed Gul Mohamed , Aayushman Sharma , Suman Chakravorty

Optimization of low-thrust trajectories that involve a larger number of orbit revolutions is considered a challenging problem. This paper describes a high-precision symplectic method and optimization techniques to solve the minimum-energy…

空间物理 · 物理学 2019-09-19 Zhibo E , Davide Guzzetti

A nonparametric adaptive controller is proposed for crane control where the payload tracks a desired trajectory with feedback from the payload position. The controller is based on a novel version of partial feedback linearization where the…

机器人学 · 计算机科学 2025-10-07 Torbjørn Smith , Olav Egeland

Soft landing on small celestial bodies (SCBs) poses unique challenges, as gravitational models poorly characterize the higher-order gravitational effects of SCBs. Existing control approaches lack guarantees for safety under gravitational…

系统与控制 · 电气工程与系统科学 2026-03-16 Felipe Arenas-Uribe , T. Michael Seigler , Jesse B. Hoagg

This paper addresses the lack of a general methodology for the controller synthesis of an optical instrument on-board a stratospheric balloon-borne platform, such as a telescope or siderostat, to meet pointing requirements that are becoming…

系统与控制 · 电气工程与系统科学 2025-11-20 Ervan Kassarian , Francesco Sanfedino , Daniel Alazard , Johan Montel , Charles-Antoine Chevrier

This study presents a framework to guarantee safety for a class of second-order nonlinear systems under multiple state and input constraints. To facilitate real-world applications, a safety-critical controller must consider multiple…

系统与控制 · 电气工程与系统科学 2023-08-09 Donggeon David Oh , Dongjae Lee , H. Jin Kim

This paper shows how to find lower bounds on, and sometimes solve globally, a large class of nonlinear optimal control problems with impulsive controls using semi-definite programming (SDP). This is done by relaxing an optimal control…

最优化与控制 · 数学 2011-10-18 Mathieu Claeys , Denis Arzelier , Didier Henrion , Jean-Bernard Lasserre

We propose a machine learning enhanced algorithm for solving the optimal landing problem. Using Pontryagin's minimum principle, we derive a two-point boundary value problem for the landing problem. The proposed algorithm uses deep learning…

最优化与控制 · 数学 2022-03-15 Yaohua Zang , Jihao Long , Xuanxi Zhang , Wei Hu , Weinan E , Jiequn Han

This paper presents an input-constrained nonlinear guidance law to address the problem of intercepting a stationary target in contested environments with multiple defending agents. Contrary to prior approaches that rely on explicit…

系统与控制 · 电气工程与系统科学 2025-09-30 Praveen Kumar Ranjan , Abhinav Sinha , Yongcan Cao

This paper deals with the problem of angle-of-attack modulation with the aim of enhancing transient performance of entry guidance during bank reversals, while compensating adverse effects of fast time-varying transient disturbances. An…

系统与控制 · 计算机科学 2016-06-09 Ran Zhang , Huifeng Li , Rui Zhang

We propose a model predictive control (MPC) based approach to a flock control problem with obstacle avoidance capability in a leader-follower framework, utilizing the future trajectory prediction computed by each agent. We employ the…

最优化与控制 · 数学 2024-04-30 Aneek Nag , Shuo Huang , Andreas Themelis , Kaoru Yamamoto

This letter considers model predictive control of a tandem-rotor helicopter. The error is formulated using the matrix Lie group $SE_2(3)$. A reference trajectory to a target is calculated using a quartic guidance law, leveraging the…

最优化与控制 · 数学 2022-06-15 Faraaz Ahmed , Ludwik Sobiesiak , James Richard Forbes