Optimal and suboptimal terminal guidance laws with practical considerations for a short range missile against an accelerating target /
Main Author: | Bates, Carlton James |
---|---|
Language: | English |
Published: |
The Ohio State University / OhioLINK
1980
|
Subjects: | |
Online Access: | http://rave.ohiolink.edu/etdc/view?acc_num=osu1487094144433863 |
Similar Items
-
Integrated CLOS and PN Guidance for Increased Effectiveness of Surface to Air Missiles
by: Binte Fatima Tuz ZAHRA, et al.
Published: (2017-06-01) -
Guidance Optimization for Tactical Homing Missiles and Air Defense Systems
by: Yunes Sh. ALQUDSI, et al.
Published: (2018-03-01) -
COMPARATIVE ANALYSIS REGARDING SURFACE-TO-AIR MISSILES GUIDANCE IN TERMS OF USING THE THREE POINTS AND PROPORTIONAL APPROACH METHODS
by: Cristian George CONSTANTINESCU, et al.
Published: (2020-03-01) -
Ramjet Application Possibilities for Increasing Fire Range of the Multiple Launch Rocket Systems Ammunition
by: V. N. Zubov, et al.
Published: (2016-06-01) -
The History of Telemetry at White Sands Missile Range, NM
by: Montano, William G., et al.
Published: (1993)