Using feedback control to apply state variable inequality constraints /
accommodate for any errors present in the model of the
| Main Author: | |
|---|---|
| Format: | Thesis eBook |
| Language: | English |
| Published: |
[Place of publication not identified] :
[publisher not identified] ;
1996.
|
| Subjects: | |
| Online Access: | Link to OAKTrust copy |
| Summary: | accommodate for any errors present in the model of the artificially high potential energy. By letting these regions be provided in addition to limiting the range of the state both require a close-loop control law and satisfying a set of boundaries, the system will inherently be repelled from the coincide with the location of the state constraint constraint limits. The other technique will define the constraints into the control law. Fortunately, there exists control law to allow a satellite to autonomously perform a controller as a cascade-saturation function, which is described as a nested series of saturation functions. By detail. The first approach supplements a Lyapunov function equations which are constraining the state variables. feedback controller capable of constraining the state given constrained rotational maneuver. illustrate the capabilities of these methods, two typical loop control law is often used since it can easily mounting it on a flexible support, and the other example is physical constraints. The first system involves alleviating physical systems are also provided, and these systems will relatively easy or logical approach to incorporate these selecting this particular definition, global stability will system. In addition to containing the equations of motion, the model may also have to satisfy a set of inequality the vibratory loads placed upon a satellite during launch by to incorporate angular constraints into a general attitude To successfully control a large variety of systems, a close- two methods that provide a better approach to developing a Unfortunately, most available methods do not provide a variables when Lyapunov analysis is performed. To help variables, and these two methods will be discussed in more with an artificial potential function to create regions of |
|---|---|
| Item Description: | "Major subject: Aerospace Engineering". Vita. |
| Physical Description: | x, 84 leaves : illustrations ; 28 cm. Also available online. Issued also on microfiche from Lange Micrographics. |
| Bibliography: | Includes bibliographical references. |