Guidance control of a missile with noisy inertial sensors

Download
093048.pdf
2000
Yıldırım, Ali Galip
Show full item record
158
views
0
downloads
https://hdl.handle.net/11511/6111
Graduate School of Natural and Applied Sciences, Thesis

Suggestions

Guidance and control of a submarine-launched cruise missile
Köklücan, Semih; Leblebicioğlu, M. Kemal.; Department of Electrical and Electronics Engineering (2019)
A typical mission profile of submarine-launched cruise missiles begins with the launch phase which covers the motion of the missile from the launch to the water-exit and continues with the boost phase which lasts from the water-exit to the beginning of the cruise phase. In order to achieve the desired range of the launch and boost phases, efficient utilization of available energy which carries the missile to the beginning of the cruise phase is necessary. For this purpose, this study presents a new approach...
Guidance and control of a spinning missile
Semerci, Bülent; Tekinalp, Ozan; Department of Aeronautical Engineering (2000)
Stabilization and orientation control of a tank gun
Şahin, Süreyya; Özgören, Kemal; Department of Mechanical Engineering (2000)
Thrust vector control of a rocket vehicle associated with aerodynamic control
Kaya, Cumhur Yalçın; Özgören, M. Kemal; Department of Mechanical Engineering (1989)
Aerodynamic optimization of missile external configurations
Arslan, Kıvanç; Özgen, Serkan; Department of Aerospace Engineering (2014)
In this thesis, design optimization methods capable of optimizing aerodynamic performances of missiles and rockets are developed. Sequential Quadratic Programming (SQP) and Random Search (RS) methods are used for optimization, whereas Missile DATCOM, which is a semi-empirical aerodynamic analysis tool, is used to calculate aerodynamic coefficients of missile configurations. As the first part of the work, capabilities and limitations of SQP and RS optimization methods are investigated on a complex test funct...
Citation Formats
A. G. Yıldırım, “Guidance control of a missile with noisy inertial sensors,” Middle East Technical University, 2000.
METU IIS - Integrated Information Service open@metu.edu.tr