Research in and application of state variable feedback design of guidance control systems for aerospace vehicles Progress report [PDF]
Weighted least squares parameter estimation, Kalman filter, and random search problems for aerospace guidance control system ...
Stefani, R. T. +2 more
core +1 more source
Parallel computations and control of adaptive structures [PDF]
The equations of motion for structures with adaptive elements for vibration control are presented for parallel computations to be used as a software package for real-time control of flexible space structures.
Alvin, Kenneth F. +5 more
core +1 more source
Systems and controls laboratory [PDF]
Advanced aerospace systems and control including thrust modulation, optimizer research, fluidic devices, hydraulic jet valves, and related ...
core +1 more source
Experimental Validation of a Sliding Mode Control for a Stewart Platform Used in Aerospace Inspection Applications [PDF]
Javier Velasco +4 more
openalex +1 more source
Safety, Trust, and Ethics Considerations for Human-AI Teaming in Aerospace Control [PDF]
Kerianne L. Hobbs, Bernard Li
openalex +1 more source
Towards sub-optimal stochastic control of partially observable stochastic systems [PDF]
A class of multidimensional stochastic control problems with noisy data and bounded controls encountered in aerospace design is examined. The emphasis is on suboptimal design, the optimality being taken in quadratic mean sense. To that effect the problem
Ruzicka, G. J.
core +1 more source
A holistic analysis method to assess the controllability of commercial buildings and their systems [PDF]
This paper describes a novel design process for advanced MIMO (multiple inputs and multiple outputs) control system design and simulation for buildings. The paper describes the knowledge transfer from high technology disciplines such as aerospace flight ...
Counsell, John M., Khalid, Yousaf A.
core
Analysis of flight data from a High-Incidence Research Model by system identification methods [PDF]
Data partitioning and modified stepwise regression were applied to recorded flight data from a Royal Aerospace Establishment high incidence research model. An aerodynamic model structure and corresponding stability and control derivatives were determined
Batterson, James G., Klein, Vladislav
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Issues in NASA program and project management [PDF]
This volume is the third in an ongoing series on aerospace project management at NASA. Articles in this volume cover the attitude of the program manager, program control and performance measurement, risk management, cost plus award fee contracting ...
Hoban, Francis T.
core +4 more sources
A high-precision attitude control satellite uses an angular momentum exchange device such as a flywheel or a control moment gyro as the actuator for attitude stability control.
Hong Zhu +6 more
doaj +1 more source

