On the inverse optimal control problem in manual control systems.
Optimal control theory with emphasis on inverse problem of finding conditions under which given manual system is optimum
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Optimal control theory with emphasis on inverse problem of finding conditions under which given manual system is optimum
Mathematical models used for space vehicle flight adaptive control systems
Analysis and design of attitude control systems for earth orbiting satellite
This paper addresses the problem of controlling a maniupulator in compliant motion while in contact with an environment having an unknown stiffness.
This paper addresses the problem of controlling a manipulator in compliant motion while in contact with an environment having an unknown stiffness.
A simulation and analysis approach is introduced for verification of attitude control flight software performance in a deep space mission.
This report is dedicated to the application of localized AFC on the NASA CRM-HL wind tunnel model, with focus on the aileron application discussed in the CFD study (final report document #2). The experience developed for the Reference Aircraft guided the implementation on the CRM model. CFD evaluations are performed on a representative high-lift configuration, for a set of aileron deflections, and at relevant flow conditions. Alternative flow control actuator layouts are proposed and design consideration for practical integration into the existing CRM-HL model are set forth. The CFD simulations indicate that the aerodynamic performance improvements due to AFC obtained for the CRM-HL are consistent with those achieved for the Reference Aircraft. The observed changes in L/D are smaller than for the Reference Aircraft because the CRM has a higher leading edge sweep angle and a different relative aileron size. Conceptual design studies confirmed that the integration of an AFC equipped aileron into the existing wind tunnel model is feasible.
This paper presents the laboratory evaluation of a commercial Microgrid Management System (MGMS) implemented in the real-world Bronzeville Microgrid which features a futuristic scenario with high renewable energy integration and the use of multiple Grid-Forming (GFM) inverters. The primary objective of the performance evaluation for the MGMS is to assess the MGMS's capability to dispatch GFM units, including a GFM PV unit and two GFM battery units, to maintain the system stability and ensure economic operation, thus guaranteeing the microgrid's resilience during prolonged outages and dynamic events. The laboratory controller hardware-in-the-loop provides realistic testing environment through detailed electromagnetic transient modeling of the microgrid system, hardware MGMS, and standard communication protocols (DNP3). The CHIL evaluation shows how the MGMS effectively manages the GFM inverters, highlighting its performance in maintaining stability, reliability, and survivability in a microgrid environment with a high penetration of renewable energy sources.
Accelerating-limiting controls for turbojet engines
Biocontrol systems - mathematical models for human manual control system through computer simulation and servoanalysis
Automatic control systems and electric measurement of nonelectric quantities in data processing related to theoretical considerations, space flights, and production engineering
Stability properties of Centaur propellant utilization control system
Second Method of Liapunov, Popov frequency criterion, and matrix inequality method used to study stability of nonlinear and/or time dependent control systems
Transonic flutter derivatives for unswept wing control surface configurations determined by pressure cell measurements
Control system for water moderated reactor using helium-3 gas
Computer simulation techniques to study proposed attitude control methods
Closed-loop compensatory tracking for measuring operator delay time in control action
Control system concept using helium 3 in water- moderated reactor