This thesis studies the equations of an uncontrolled unguided anti-tank missile with six-degree-of-freedom. The main aspect of this study is to include the internal ballistic effects in the equations of motion. Due to the approach which is adopted to drive the equations of motion of the missile, the internal ballistic terms appear explicitly with the external ballistic terms in a Unified Equations of Motion
Multibody modeling of an internal gyroscopic micro-mechanism for development of lateral deviation of...
In this paper, the question of the motion of a projectile thrown at an angle to the horizon is learn...
In this study, the dynamic modeling, guidance, and control of a missile with two relatively rotating...
This thesis studies the equations of an uncontrolled unguided anti-tank missile with six-degree-of-f...
This paper contains an analysis of a mathematical model of a missile which is initially at rest in f...
This report contains a general formulation of the equations of motion for a rocket consisting of two...
W pracy przedstawiono sposób konstruowania modelu matematycznego dynamiki lotu pocisków stabilizowan...
A general formulation of the dynamical problems associated with powered flight of a two stage flexib...
International Series of Monographs on Aeronautics and Astronautics, Division VII, Volume 5: The Flig...
In the paper the three different mathematical models of motion of a spin-stabilized, conventional ar...
Abstract: The paper presents the relations that form the basis for the calculus models needed to stu...
AbstractThis article investigates the dynamic characteristics of deflectable nose missiles with rota...
Przedmiotem pracy była weryfikacja rozwiązania głównego problemu balistyki zewnętrznej dla pocisku b...
This report contains a restatement of the equations governing the exterior ballistics of a free flig...
Click on the DOI link to access the article (may not be free).The lateral control of a projectile fo...
Multibody modeling of an internal gyroscopic micro-mechanism for development of lateral deviation of...
In this paper, the question of the motion of a projectile thrown at an angle to the horizon is learn...
In this study, the dynamic modeling, guidance, and control of a missile with two relatively rotating...
This thesis studies the equations of an uncontrolled unguided anti-tank missile with six-degree-of-f...
This paper contains an analysis of a mathematical model of a missile which is initially at rest in f...
This report contains a general formulation of the equations of motion for a rocket consisting of two...
W pracy przedstawiono sposób konstruowania modelu matematycznego dynamiki lotu pocisków stabilizowan...
A general formulation of the dynamical problems associated with powered flight of a two stage flexib...
International Series of Monographs on Aeronautics and Astronautics, Division VII, Volume 5: The Flig...
In the paper the three different mathematical models of motion of a spin-stabilized, conventional ar...
Abstract: The paper presents the relations that form the basis for the calculus models needed to stu...
AbstractThis article investigates the dynamic characteristics of deflectable nose missiles with rota...
Przedmiotem pracy była weryfikacja rozwiązania głównego problemu balistyki zewnętrznej dla pocisku b...
This report contains a restatement of the equations governing the exterior ballistics of a free flig...
Click on the DOI link to access the article (may not be free).The lateral control of a projectile fo...
Multibody modeling of an internal gyroscopic micro-mechanism for development of lateral deviation of...
In this paper, the question of the motion of a projectile thrown at an angle to the horizon is learn...
In this study, the dynamic modeling, guidance, and control of a missile with two relatively rotating...