Agile Missile Dynamics and Control
| Autor: | David J. B Roy, Kevin A. Wise |
|---|---|
| Rok vydání: | 1998 |
| Předmět: |
Engineering
business.industry Angle of attack Applied Mathematics Aerospace Engineering Missile guidance Aerodynamics Reaction control system law.invention Computer Science::Robotics Missile Flight envelope Computer Science::Systems and Control Space and Planetary Science Control and Systems Engineering law Autopilot Electrical and Electronic Engineering Aerospace engineering business Thrust vectoring |
| Zdroj: | Journal of Guidance, Control, and Dynamics. 21:441-449 |
| ISSN: | 1533-3884 0731-5090 |
| Popis: | This paper discusses the dynamics and control of missiles capable of high angle of attack flight. The missile control effectors discussed include thrust vectoring, reaction jet thrusters, and aerodynamic tail surfaces. A control power analysis that indicates the effectiveness of these control effectors over the missile's flight envelope is summarized. The 6-DOF dynamics for high angle of attack missile flight control are presented. Autopilot design models and nonlinear simulation results demonstrating high angle of attack flight are also presented. (Author) |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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