This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Missile Control System Design and Specification for a Long-Range Supersonic Cruise Missile
Technical Paper
2005-01-3379
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
This paper presents an overview of two long-range supersonic cruise missile prototypes and the preliminary design of the Missile Control System (MCS). The MCS provides command and control of all flight-critical subsystems. It is responsible for aerodynamic effector, propulsion flowpath, and embedded digital engine control. The flowpath control system, based on the SR-71flowpath design, includes a movable inlet spike, engine bypass flow control, and ram burner inlet flow valve. The engine controller provides all High Speed Turbojet engine effector commands: variable inlet guide vanes, fuel pumps, and movable exhaust spike. System development leverages model-based specification, design, integration, and verification & validation testing.
Recommended Content
| Aerospace Standard | Numerical Modeling Techniques for Jet Engine Test Cell Aerodynamics |
| Aerospace Standard | In-Flight Thrust Determination |
| Aerospace Standard | Real-Time Modeling Methods for Gas Turbine Engine Performance |
Citation
Hostetler, J., "Missile Control System Design and Specification for a Long-Range Supersonic Cruise Missile," SAE Technical Paper 2005-01-3379, 2005, https://doi.org/10.4271/2005-01-3379.Also In
References
- YF-12A Dynamic Inlet Computer Program User's Manual Lockheed Aircraft Corporation Advanced Development Projects Burbank, CA 1971
- Model-Based Design Framework For the Development of Flight Controls/Vehicle Management Operational Real-Time Software using Matlab, Simulink & RTW Vu Thu-Nga Flight Controls / Vehicle Management Systems Lockheed Martin Aeronautics Company Fort Worth, TX 2002
- SDIF SDD Flight Control Applications Simulink Modeling Standards, Revision 1 Advanced Development Programs Lockheed Martin Aeronautics Company Fort Worth, TX 2004
- Digital Control of Dynamic Systems Franklin Gene F. Powell J. David Workman Michael Prentice Hall 3rd 1997
- Dynamics of Flight Etkin Bernard Reid Lloyd Duff Wiley 3rd 1995