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Flight Control with and without Control Surfaces: A Nonlinear Look
| Content Provider | Scilit |
|---|---|
| Author | Sivasundaram, S. |
| Copyright Year | 2000 |
| Description | Aircraft flight control systems are traditionally designed based on linearized dynamics and linear control methodologies [1]. While the linear designs have been remarkably successful, increasingly high performance of modem aircraft, usually associated with large flight envelope, high angle of attack and large angular rates, has invalidated the fundamental assumption of small perturbations of linearization. In these conditions the nonlinearity in the aircraft dynamics becomes so prominent that it can no longer be ignored. A satisfactory flight control system must take into account the inherent nonlinearity dictated by the law of physics. Book Name: Nonlinear Problems in Aviation and Aerospace |
| Related Links | https://content.taylorfrancis.com/books/download?dac=C2004-0-11740-5&isbn=9780429182006&doi=10.1201/9781482296914-16&format=pdf |
| Ending Page | 156 |
| Page Count | 16 |
| Starting Page | 141 |
| DOI | 10.1201/9781482296914-16 |
| Language | English |
| Publisher | Informa UK Limited |
| Publisher Date | 2000-01-10 |
| Access Restriction | Open |
| Subject Keyword | Book Name: Nonlinear Problems in Aviation and Aerospace Aerospace Engineering Control Systems Nonlinearity Aircraft Flight Control System Modem Angular Inherent Ignored |
| Content Type | Text |
| Resource Type | Chapter |
