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With quadrotor use seeing extensive growth in recent years, the autonomous control of these Unmanned Aerial Vehicles (UAVs) is an increasing relevant and intersting field. In this paper a linear state-space approach at designing a stable…

系统与控制 · 计算机科学 2014-10-03 Graeme N. Wilson , Alejandro Ramirez-Serrano , Qiao Sun

In this paper, we present a cascade control structure to address the trajectory tracking problem for quadcopters, ensuring uniform global asymptotic stability of the state tracking error dynamics. An MPC strategy based on a 12-dimensional…

系统与控制 · 电气工程与系统科学 2025-09-03 Maedeh Izadi , A. T. J. R. Cobbenhagen , R. L. Sommer , A. R. P. Andrien , E. Lefeber , W. P. M. H. Heemels

Tiltrotors are an aircraft concept with the ability to rotate their rotors freely, achieving vertical take-off and fast forward flight. The combination of helicopter and fixed-wing flight into one aircraft provides versatility in mission…

系统与控制 · 电气工程与系统科学 2024-11-12 George Kirst , Xinhua Wang

This paper presents a flight control design for compound Vertical Takeoff and Landing (VTOL) vehicles. With their multitude of degrees of controllability as well as the significant variations in their flight characteristics, VTOL vehicles…

系统与控制 · 电气工程与系统科学 2024-05-28 Jean-Marie Kai

MAVs have great potential to assist humans in complex tasks, with applications ranging from logistics to emergency response. Their agility makes them ideal for operations in complex and dynamic environments. However, achieving precise…

机器人学 · 计算机科学 2025-10-30 Luis F. Recalde , Dhruv Agrawal , Jon Arrizabalaga , Guanrui Li

Fault tolerance is achieved through multiply redundant hardware systems in large civil aircraft. This means of achieving fault tolerance is infeasible for small compact unmanned aerial vehicles. In this paper we apply a fault tolerant…

最优化与控制 · 数学 2016-10-12 Rudaba Khan , Paul Williams , Paul Riseborough , Asha Rao , Robin Hill

Autonomous unpowered flight is a challenge for control and guidance systems: all the energy the aircraft might use during flight has to be harvested directly from the atmosphere. We investigate the design of an algorithm that optimizes the…

机器学习 · 计算机科学 2017-07-19 Erwan Lecarpentier , Sebastian Rapp , Marc Melo , Emmanuel Rachelson

Quadrotors are indispensable in civilian, industrial, and military domains, undertaking complex, high-precision tasks once reserved for specialized systems. Across all contexts, energy efficiency remains a critical constraint: quadrotors…

系统与控制 · 电气工程与系统科学 2025-08-29 Daniel Engelsman , Itzik Klein

With quadrotors becoming immensely popular in applications such as relief operations, infrastructure maintenance etc., a key control design challenge arises when the quadrotor has to manoeuvre through constrained spaces during various…

系统与控制 · 电气工程与系统科学 2022-01-12 Sourish Ganguly

Traditional aerial vehicles are usually custom-designed for specific tasks. Although they offer an efficient solution, they are not always able to adapt to changes in the task specification, e.g., increasing the payload. This applies to…

机器人学 · 计算机科学 2022-01-25 Jiawei Xu , Diego S. D'Antonio , David Saldaña

This paper introduces a learning-based low-level controller for quadcopters, which adaptively controls quadcopters with significant variations in mass, size, and actuator capabilities. Our approach leverages a combination of imitation…

机器人学 · 计算机科学 2025-06-10 Dingqi Zhang , Antonio Loquercio , Jerry Tang , Ting-Hao Wang , Jitendra Malik , Mark W. Mueller

This paper explains the integration process of an autonomous quadcopter platform and the design of Arduino based novel software architecture that enables the execution of advanced control laws on low-cost off-the-shelf products based…

最优化与控制 · 数学 2015-08-21 Ankyda Ji , Kamran Turkoglu

A major challenge in autonomous flights is unknown disturbances, which can jeopardize safety and lead to collisions, especially in obstacle-rich environments. This paper presents a disturbance-aware motion planning and control framework…

Isoperimetric robotic trusses can adapt to different tasks and environments because they have a high strength-to-weight ratio, can change their own shape dramatically, and can be reconfigured into a variety of different shapes. However,…

机器人学 · 计算机科学 2026-05-21 James Wade , Isaac Weaver , Mihai Stanciu , Nathan Usevitch

Proportional-Integrator-Derivative (PID) controller is used in a wide range of industrial and experimental processes. There are a couple of offline methods for tuning PID gains. However, due to the uncertainty of model parameters and…

系统与控制 · 电气工程与系统科学 2025-08-19 Iman Sharifi , Aria Alasty

Despite extensive research on sliding mode control (SMC) design for quadrotors, the existing approaches suffer from certain limitations. Euler angle-based SMC formulations suffer from poor performance in high-pitch or -roll maneuvers.…

机器人学 · 计算机科学 2025-12-04 Amin Yazdanshenas , Reza Faieghi

This paper describes the design process for developing a nonlinear model predictive controller for fault tolerant flight control. After examining and implementing a number of numerical techniques, this paper identifies pseudospectral…

最优化与控制 · 数学 2016-10-10 Rudaba Khan , Paul Williams , Paul Riseborough , Asha Rao , Robin Hill

Three-dimensional integration technologies such as flip-chip bonding are a key prerequisite to realize large-scale superconducting quantum processors. Modular architectures, in which circuit elements are spread over multiple chips, can…

Two-dimensional multilinked structures can benefit aerial robots in both maneuvering and manipulation because of their deformation ability. However, certain types of singular forms must be avoided during deformation. Hence, an additional 1…

机器人学 · 计算机科学 2023-01-11 Moju Zhao , Tomoki Anzai , Kei Okada , Masayuki Inaba

This work addresses the problem of robust attitude control of quadcopters. First, the mathematical model of the quadcopter is derived considering factors such as nonlinearity, external disturbances, uncertain dynamics and strong coupling.…

系统与控制 · 计算机科学 2018-06-06 V. T. Hoang , M. D. Phung , Q. P. Ha