Parametric study of guidance of a 160-mm projectile steered with lateral thrusters
R Głębocki, M Jacewicz - Aerospace, 2020 - mdpi.com
The development of projectile guidance requires consideration of a large number of
possible flight scenarios with various system parameters. In this paper, the Monte-Carlo …
possible flight scenarios with various system parameters. In this paper, the Monte-Carlo …
[PDF][PDF] Impact point prediction guidance parametric study for 155 mm rocket assisted artillery projectile with lateral thrusters
A Szklarski, R Głębocki… - Archive of mechanical …, 2020 - bibliotekanauki.pl
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 …
thrusters was proposed. Six degree of freedom mathematical model was used to investigate …
Ballistic missile trajectory prediction and the solution algorithms for impact point prediction
X Zhang, HM Lei, J Li, DY Zhang - Proceedings of 2014 IEEE …, 2014 - ieeexplore.ieee.org
In order to improve the guidance precision of the ballistic missile interception, the target's
trajectory prediction and the impact point prediction solution algorithm for interceptor's mid …
trajectory prediction and the impact point prediction solution algorithm for interceptor's mid …
Monte-Carlo based lateral thruster parameters optimization for 122 mm rocket
M Jacewicz, R Glebocki, R Ozog - Conference on Automation, 2020 - Springer
One of the current tendencies is to equip the unguided munition designed for ballistic
shooting with low cost, solid propellant lateral thrusters based, actuators to achieve the …
shooting with low cost, solid propellant lateral thrusters based, actuators to achieve the …