標(biāo)題: Titlebook: Control of Autonomous Aerial Vehicles; Advances in Autopilo Andrea L‘Afflitto,Gokhan Inalhan,Hyo-Sang Shin Book 2024 The Editor(s) (if appl [打印本頁(yè)] 作者: CT951 時(shí)間: 2025-3-21 16:17
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書目名稱Control of Autonomous Aerial Vehicles讀者反饋學(xué)科排名
作者: liaison 時(shí)間: 2025-3-21 21:37 作者: 干旱 時(shí)間: 2025-3-22 01:42 作者: Protein 時(shí)間: 2025-3-22 08:16
https://doi.org/10.1007/978-3-031-39767-7Unmanned Aerial Vehicles; Guidance, Navigation and Control; Optimal Control; Nonlinear Control; Aerial R作者: 史前 時(shí)間: 2025-3-22 08:48
978-3-031-39769-1The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl作者: 公理 時(shí)間: 2025-3-22 13:20
Andrea L‘Afflitto,Gokhan Inalhan,Hyo-Sang Shin? Tutorial style of chapters assists the reader in understanding the material presented.A benchmark for the state-of-the-art in UAV systems design including for urban air mobility.Careful organization作者: 公理 時(shí)間: 2025-3-22 17:52 作者: exophthalmos 時(shí)間: 2025-3-22 21:32 作者: surmount 時(shí)間: 2025-3-23 01:30 作者: 不能約 時(shí)間: 2025-3-23 09:10
Ralf T. Kreutzer,Darius Seyed Vousoghitasked with creating maps of unknown environments while operating in a tactical manner and at very low altitudes. The few existing guidance systems for UAVs operating in potentially hazardous environments essentially assume direct information on the location and the kind of potential threat to the a作者: EWER 時(shí)間: 2025-3-23 11:01 作者: languid 時(shí)間: 2025-3-23 15:07
Wolfgang Haller,Sabrina Stiegerrtification, there is a strong desire to compare the new algorithms with the ones used for more conventional aircraft such as turbofan fixed-wing vehicles. With this need in mind, the main contribution of this chapter is to propose a unified approach for the maximum endurance of turbojet, turboprop,作者: dearth 時(shí)間: 2025-3-23 21:19 作者: Scintillations 時(shí)間: 2025-3-23 22:39
VOB/A 2019 - Textausgabe/Text Editionangerous situations. This chapter proposes a safety-constrained control framework that adapts UAVs at a path re-planning level to support resilient state estimation in GPS-denied environments. The proposed framework consists of an anomaly detector, a resilient state estimator, a robust controller, a作者: motivate 時(shí)間: 2025-3-24 05:42
https://doi.org/10.1007/978-3-658-29622-3peed becomes a challenging task due to unmodeled aerodynamic forces and moments. In this study, position and attitude tracking controllers are presented in a structured cascaded fashion using incremental nonlinear dynamic inversion (INDI). A new approach for yaw rotational dynamic INDI control law i作者: 用手捏 時(shí)間: 2025-3-24 06:42 作者: 招待 時(shí)間: 2025-3-24 11:55 作者: 破布 時(shí)間: 2025-3-24 17:31 作者: endarterectomy 時(shí)間: 2025-3-24 22:08
VOB/B 2019 - Textausgabe/Text Editionders an aerial device with tilting propellers that, thanks to a super-twisting slide mode controller, can control the interaction force for inspection task purposes. The latter proposes a hardware-in-the-loop simulator for human cooperation and environmental interaction with an aerial manipulator. T作者: linguistics 時(shí)間: 2025-3-25 00:17 作者: monochromatic 時(shí)間: 2025-3-25 07:03
1430-9491 eaders who are researchers, practitioners or graduate students in control theory, autonomous systems or robotics, or in aerospace, mechanical or electrical engineering..978-3-031-39769-1978-3-031-39767-7Series ISSN 1430-9491 Series E-ISSN 2193-1577 作者: doxazosin 時(shí)間: 2025-3-25 11:25
Book 2024ts of which are discussed in detail..Control of Autonomous AerialVehicles.?will interest readers who are researchers, practitioners or graduate students in control theory, autonomous systems or robotics, or in aerospace, mechanical or electrical engineering..作者: Slit-Lamp 時(shí)間: 2025-3-25 13:07 作者: 孤僻 時(shí)間: 2025-3-25 18:11 作者: Peak-Bone-Mass 時(shí)間: 2025-3-25 23:55 作者: 眼界 時(shí)間: 2025-3-26 00:15 作者: muffler 時(shí)間: 2025-3-26 05:50
Incremental Control to Reduce Model Dependency of Classical Nonlinear Control,g the state derivative and control input measurements. A closed-loop analysis with IBKS is conducted for three different cases. In the first test case, which involves model uncertainties and ideal measurements, unlike BKS, the closed-loop stability and performance of IBKS are not affected if the con作者: 感染 時(shí)間: 2025-3-26 09:57
Ralf T. Kreutzer,Darius Seyed Vousoghice system can be employed by first responders and other emergency units to collect real-time data about a given location. Several unique features distinguish the proposed guidance system, including an original algorithm to cover connected set, which allows users to prioritize accuracy over flight ti作者: 單片眼鏡 時(shí)間: 2025-3-26 14:56 作者: Vldl379 時(shí)間: 2025-3-26 17:09
https://doi.org/10.1007/978-3-658-29500-4e source term in turbulent and noisy environments are presented using domain knowledge such as the plume dispersion and sensor models. In particular, since the estimation problem is highly nonlinear and non-Gaussian, the sequential Monte Carlo method (i.e., particle filter) Besides, various informat作者: 失望昨天 時(shí)間: 2025-3-26 23:11 作者: 色情 時(shí)間: 2025-3-27 04:40
VOB/A 2019 - Textausgabe/Text Editiong the state derivative and control input measurements. A closed-loop analysis with IBKS is conducted for three different cases. In the first test case, which involves model uncertainties and ideal measurements, unlike BKS, the closed-loop stability and performance of IBKS are not affected if the con作者: 翅膀拍動(dòng) 時(shí)間: 2025-3-27 09:18
https://doi.org/10.1007/978-3-658-29460-1tonomy in complex, dynamic environments. In this chapter, we briefly outline some key aspects of the state of UAV technology. Successively, by providing the outline of this book, we explain in what directions research has been steered to address key shortcomings of UAVs for civilian applications.作者: Hiatal-Hernia 時(shí)間: 2025-3-27 13:24
VOB/B 2019 - Textausgabe/Text Editionhis part includes the mathematical background and theoretical derivation with insights into the relative stability proofs. Simulations in a highly realistic environment endowed with a physics engine and real experiments validate both the proposed approaches.作者: 拋射物 時(shí)間: 2025-3-27 17:32
1430-9491 design including for urban air mobility.Careful organization.Control of Autonomous Aerial Vehicles.?is an edited book that provides a single-volume snapshot on the state of the art in the field of control theory applied to the design of autonomous unmanned aerial vehicles (UAVs), aka “drones”, emplo作者: figure 時(shí)間: 2025-3-27 19:48 作者: DEAF 時(shí)間: 2025-3-28 01:06
https://doi.org/10.1007/978-3-658-29460-1he prediction of the trajectory of a nonlinear system over a receding time horizon from the current time and the generation of the control input sequences by solving the given optimal control problem. Numerical simulation demonstrates the effectiveness of the NMPC-based guidance algorithm compared with other benchmark guidance schemes.作者: 柱廊 時(shí)間: 2025-3-28 05:52
Nonlinear Model Predictive Controller-Based Line Tracking Guidance,he prediction of the trajectory of a nonlinear system over a receding time horizon from the current time and the generation of the control input sequences by solving the given optimal control problem. Numerical simulation demonstrates the effectiveness of the NMPC-based guidance algorithm compared with other benchmark guidance schemes.作者: 不整齊 時(shí)間: 2025-3-28 09:08 作者: FLINT 時(shí)間: 2025-3-28 10:25
https://doi.org/10.1007/978-3-658-29622-3vement over the legacy proportional-integral-derivative (PID) controller is shown in outdoor flight tests. Circle and lemniscate-shaped trajectories are tracked with a maximum speed of 15?m/s. The attitude hold and tracking performance are evaluated with a maximum speed of 30?m/s.作者: 纖細(xì) 時(shí)間: 2025-3-28 15:27 作者: 幻想 時(shí)間: 2025-3-28 20:58
VOB/B 2019 - Textausgabe/Text Editiontwo problems is achieved by a new decoupling virtual tracking error (that is, information exchange between agents). A numerical example demonstrates an application of the proposed approach to a heterogeneous multi-vehicle system consisting of unmanned aerial and ground vehicles in formation.作者: elastic 時(shí)間: 2025-3-28 23:05 作者: 寬度 時(shí)間: 2025-3-29 05:05
Incremental Nonlinear Dynamic Inversion-Based Trajectory Tracking Controller for an Agile Quadrotorvement over the legacy proportional-integral-derivative (PID) controller is shown in outdoor flight tests. Circle and lemniscate-shaped trajectories are tracked with a maximum speed of 15?m/s. The attitude hold and tracking performance are evaluated with a maximum speed of 30?m/s.作者: MUMP 時(shí)間: 2025-3-29 07:42
Adaptive Dynamic Programming for Flight Control, of a type that is not anticipated during the control design. This chapter first gives a brief historical overview of ADP applications to flight control tasks. After that, four recent advances of ADP for flight control are presented.作者: Cerumen 時(shí)間: 2025-3-29 12:17
A Distributed Adaptive Control Approach to Cooperative Output Regulation of a Class of Heterogeneoutwo problems is achieved by a new decoupling virtual tracking error (that is, information exchange between agents). A numerical example demonstrates an application of the proposed approach to a heterogeneous multi-vehicle system consisting of unmanned aerial and ground vehicles in formation.作者: 左右連貫 時(shí)間: 2025-3-29 18:38
Introduction,tonomy in complex, dynamic environments. In this chapter, we briefly outline some key aspects of the state of UAV technology. Successively, by providing the outline of this book, we explain in what directions research has been steered to address key shortcomings of UAVs for civilian applications.作者: cinder 時(shí)間: 2025-3-29 22:31 作者: 規(guī)范就好 時(shí)間: 2025-3-30 02:30
Introduction,such as collecting images and videos, these vehicles are not yet employed in more complex tasks as it would have been envisioned a decade ago. The reasons for this state-of-the-art are numerous, and mostly to be sought in the need for advanced guidance, navigation, and control systems that enable au作者: SOW 時(shí)間: 2025-3-30 05:21
Nonlinear Model Predictive Controller-Based Line Tracking Guidance, The guidance problem is formulated in the nonlinear model predictive control (NMPC) framework with a nonlinear discrete-time kinematics model. The derived error dynamics with respect to the flight path are solved by numerical optimization minimizing the associated performance index in conjunction w作者: MEAN 時(shí)間: 2025-3-30 08:53 作者: 無(wú)法取消 時(shí)間: 2025-3-30 13:20 作者: Neutropenia 時(shí)間: 2025-3-30 19:27 作者: Pantry 時(shí)間: 2025-3-30 23:02
