Computer display and control for launch vehicles.
Computer display and control system for launch vehicle test operation
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Computer display and control system for launch vehicle test operation
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Spacecraft guidance and control systems during rendezvous and docking
Sensitivity theory for design of spacecraft flight control systems
Trajectory equations describing spacecraft motion from launch to earth impact or orbit injection
Sensing, signal processing, and actuation functions of spacecraft flight control
Analysis and design of attitude control systems for earth orbiting satellite
Manned spacecraft control system requirements for abort problems
Spacecraft attitude control system using solar and earth sensors, gyroscopes, and jet actuators
Attitude control training device for astronauts permitting friction-free movement with five degrees of freedom
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System prevents tire skid during panic stops. Two mutually dependent accelerometers directly control solenoid valve which regulates braking pressure.
The control of the rendezvous vehicle during proximity operations is considered. It is shown how fuzzy sets can be used for autonomous vehicle control to model the human capability of common sense reasoning. Such models are integrated with expert systems and engineering control systems technology to create a system that performs comparably to a manned system.
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The Zenith Star Experiment is designed to demonstrate and evaluate the performance of a laser in space to answer critical issues relevant to SDI. The spacecraft design, control system architecture, and vehicle control are discussed.
Increased operational autonomy and reduced operating costs have become critical design objectives in next-generation NASA and DoD space programs. The objective is to develop a semi-automated system for intelligent spacecraft operations support. The Spacecraft Operations and Anomaly Resolution System (SOARS) is presented as a standardized, model-based architecture for performing High-Level Tasking, Status Monitoring and automated Procedure Execution Control for a variety of spacecraft. The particular focus is on the Procedure Execution Control module. A hierarchical procedure network is proposed as the fundamental means for specifying and representing arbitrary operational procedures. A separate procedure interpreter controls automatic execution of the procedure, taking into account the current status of the spacecraft as maintained in an object-oriented spacecraft model.
Progress on research on the control of actions of autonomous mobile agents using fuzzy logic is presented. The innovations described encompass theoretical and applied developments. At the theoretical level, results of research leading to the combined utilization of conventional artificial planning techniques with fuzzy logic approaches for the control of local motion and perception actions are presented. Also formulations of dynamic programming approaches to optimal control in the context of the analysis of approximate models of the real world are examined. Also a new approach to goal conflict resolution that does not require specification of numerical values representing relative goal importance is reviewed. Applied developments include the introduction of the notion of approximate map. A fuzzy relational database structure for the representation of vague and imprecise information about the robot's environment is proposed. Also the central notions of control point and control structure are discussed.