Impact point prediction guidance parametric study for 155 mm rocket assisted artillery projectile with lateral thrusters
The modified configuration of the 155 mm rocket assisted projectile equipped with lateral thrusters was proposed. Six degree of freedom mathematical model was used to investigate the quality of the considered projectile. Impact point prediction guidance scheme intended for low control authority proj...
Main Authors: | Szklarski Adrian, Głębocki Robert, Jacewicz Mariusz |
---|---|
Format: | Article |
Language: | English |
Published: |
Polish Academy of Sciences
2020-03-01
|
Series: | Archive of Mechanical Engineering |
Subjects: | |
Online Access: | http://journals.pan.pl/dlibra/publication/131682/edition/115014/content |
Similar Items
-
Parametric Study of Guidance of a 160-mm Projectile Steered with Lateral Thrusters
by: Robert Głębocki, et al.
Published: (2020-05-01) -
Sensitivity Analysis and Flight Tests Results for a Vertical Cold Launch Missile System
by: Robert Głębocki, et al.
Published: (2020-11-01) -
Naphthalene as a Cubesat Cold Gas Thruster Propellant
by: Dimitrios Tsifakis, et al.
Published: (2020-09-01) -
An Inductively-Coupled Plasma Electrothermal Radiofrequency Thruster
by: Dimitrios Tsifakis, et al.
Published: (2020-02-01) -
Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students
by: Powaser, Alexander M.
Published: (2019)