We propose a new smooth attitude controller for rigid body in the presence of input saturation and external *** controller is composed of three parts,i.e.,the quaternion part,the saturated velocity part,and the bounde...
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ISBN:
(纸本)9789881563897
We propose a new smooth attitude controller for rigid body in the presence of input saturation and external *** controller is composed of three parts,i.e.,the quaternion part,the saturated velocity part,and the bounded disturbance compensation *** disturbance compensation part is derived from disturbance *** main contribution of the study is that the constructed observers can globally asymptotically track the external disturbances,given the disturbances are twice differentiable with bounded *** are conducted to validate the effectiveness of the proposed controllers.
This paper presents a new guidance law based on sliding-mode control and input-to-state stability(ISS) for approach and landing of a reusable launch vehicle(RLV). According to the idea of reference-trajectory guidance...
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ISBN:
(纸本)9781467374439
This paper presents a new guidance law based on sliding-mode control and input-to-state stability(ISS) for approach and landing of a reusable launch vehicle(RLV). According to the idea of reference-trajectory guidance, the sliding mode surface is chosen to be a linear combination of the reference-trajectory tracking error and its rate, and a guidance law is designed to make the dynamics of the sliding mode surface be ISS with respect to bounded uncertainties. Then, by introducing class KL-like function, it is proved that the influence of uncertainties on reference-trajectory tracking error can be close to zero by adjusting the guidance parameters. The numerical simulation confirms the effectiveness of the proposed design approach.
According to task requests of deep space exploration approach phase such as autonomy, real-time and so on, we did a research into the problem of autonomous navigation at this approach phase and put forward an autonomo...
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In this paper, we study the robust design of the flight control system for the longitudinal dynamics of air-breathing hypersonic vehicles. First, the longitudinal dynamics model is divided into the velocity subsystem ...
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Online water quality monitoring systems have many significant benefits in fields such as source water protection, water treatment, and wastewater discharge, and in accidental or deliberate event of water contamination...
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Motivated by the effort to understand the mathematical structure underlying the Teukolsky equations in a Kerr metric background, a homogeneous integral equation related to the prolate spheroidal function is studied. F...
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Motivated by the effort to understand the mathematical structure underlying the Teukolsky equations in a Kerr metric background, a homogeneous integral equation related to the prolate spheroidal function is studied. From the consideration of the Fredholm determinant of the integral equation, a family of generalized error function is defined, with which the Fredholm determinant of the sinc kernel is also evaluated. An analytic solution of a special ease of the fifth Painlev~ transcendent is then worked out explicitly.
In this study,the fuel-optimal trajectory optimization problem of lunar soft landing using variable-thrust propulsion is ***,we formulate the trajectory optimization problem of lunar soft landing with three-dimensiona...
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ISBN:
(纸本)9781467383196
In this study,the fuel-optimal trajectory optimization problem of lunar soft landing using variable-thrust propulsion is ***,we formulate the trajectory optimization problem of lunar soft landing with three-dimensional kinematics and dynamics,boundary constraints,and path constraints strictly *** formulated trajectory optimization problem is then solved by the simultaneous dynamic optimization *** bounds imposed on the magnitude of the engine thrust,the optimal thrust profile typically has a "bang-bang" *** general simultaneous dynamic optimization approach has difficulty handling breakpoints of control profiles.A novel adaptive mesh refinement strategy based on a constant Hamiltonian profile is proposed to address the difficulty of locating breakpoints of the thrust *** results show that the enhanced simultaneous dynamic optimization approach with the adaptive mesh refinement strategy can effectively capture breakpoints of the optimal thrust profile and obtain more refined optimal solutions,compared with the general simultaneous dynamic optimization approach.
This paper focuses on the design of a novel SMC(servo motor controller) based on EtherCAT in order to realize flexible networked multi-axis motion control with low cost and high *** is chosen as only kernel component ...
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ISBN:
(纸本)9781467397155
This paper focuses on the design of a novel SMC(servo motor controller) based on EtherCAT in order to realize flexible networked multi-axis motion control with low cost and high *** is chosen as only kernel component of the SMC to improve the integration level of the *** with some necessary peripheral chips,those functions such as EtherCAT communication,encoder signal acquisition and processing,D/A conversion and logic I/O control can be executed independently and parallelly at high *** control algorithm is implemented to achieve the closed-loop control of a single motor by embedding Nios Ⅱ soft core in *** the application of multi-axis control,multiple SMCs as the EtherCAT slaves can be connected to an IPC(Industrial PC) as the EtherCAT master to establish a flexible networked multi-axis motion control *** on SOEM(Simple Open EtherCAT Master),the EtherCAT master program is developed in the form of dynamic link library,which can realize more advanced control algorithm to meet the needs of complex applications with the help of powerful computing ability of an *** general,the novel SMC is with the advantages of low cost,compact size,simple connection,high flexibility and good real-time performance,and expects a promising application prospect in the field of motion control.
This paper focuses on the K-COVER problem in unmanned aerial vehicle (UAV) sensor networks and proposes a game theoretic approach based on the network potential game and Log-linear learning. After detailing the resear...
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With the transformation of military tactic to informatization and networking and the need of rapid processing and measurement of mass of data,the measurement system of missile launch system is important to guarantee t...
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With the transformation of military tactic to informatization and networking and the need of rapid processing and measurement of mass of data,the measurement system of missile launch system is important to guarantee the operation to be *** order to reduce the complexity of the measurement and control system and the time of preparation before launching and increasing the level of combat,the authors build a distributed and autonomous measurement system based on B/S(Browser/Server) mode which combines the technology of virtual instrument,database,embedded system and various communications *** this system,the authors use general development tool Visual C++ to develop the background test program for underlying data collection,and use My Eclipse to design front pages to achieve remote monitoring,data display and output the analyzed statistical *** system satisfies the technical requirement after the performance testing and data acquisition *** provides a platform for the future study of data synchronization and parallel *** the same time,it is useful for the development of multi-testing nodes and large amount of data communication of complex distributed measurement system.
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