Boost Control Design for Spinning Missile

You are here: Homepage > Search

Boost Control Design for Spinning Missile

Boost Control Design for Spinning Missile

R. L. Park

A compensation scheme is presented for the pitch-yaw control system of a strategic missile which maintains stability and performance while the missile spins. The conventional missile control design for boost has uncoupled pitch, yaw and roll channels ideally suited for a non-rolling missile. The effect roll has on the conventional pitch-yaw controller is discussed and the development and simulation of a modified system is presented. Keywords: Spinning missile; and Thrust vector control.

Access

Check availability in my library

Export, share and cite

Document information

Title :

Boost Control Design for Spinning Missile

Contributors:

R. L. Park (author)

Publication date :

1985

Size :

97 pages

Type of media :

Report

Type of material :

No indication

Language :

English

Keywords :

Surface Launched Missiles , Spinning(Motion) , Boost phase , Compensation , Control , Guided missiles , Pitch(Motion) , Simulation , Thrust vector control systems , Long range(Distance) , Strategic weapons , Theses , Yaw , Surface to surface missiles

Similar titles

Boost Assisted Missile Launcher

L. J. Holt / C. Panlaqui | NTIS | 1979

Vacuum-air missile boost system

KUMAR, S. / MURRAY, J. J. / RAJAN, J. R. N. | AIAA | 1964

Time-Optimal Attitude Control Scheme for a Spinning Missile

Jahangir, E. | Online Contents | 1993

Midcourse Guidance and Control for Pulse Motor Boost Missile

Tang, Mao / Gong, Yinghui / Xie, Jia et al. | Springer Verlag | 2021

Alternatives for Boost-Phase Missile Defense

NTIS | 2004

Access

Check availability in my library

Page navigation

Document information

Export, share and cite