AbstractCompared with the one-dimensional trajectory correction technology which adjusts longitudinal range, not only does the two-dimensional trajectory correction technology adjust the force in velocity direction, but also need to modulate the lateral force or trajectory (perpendicular to the vertical plane of fire direction). Therefore, the structure of control cabin of two-dimensional trajectory correction projectile (TDTCP) is more complicated than that of one-dimensional trajectory correction projectile (ODTCP). To simplify the structure of control cabin of TDTCP and reduce the cost, a scheme of adding a damping disk to the control cabin of ODTCP has been developed recently. The damping disk is unfolded at the right moment during its ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical EngineeringThe ...
This paper presents an optimum control scheme of firing time and firing phase angle by taking impact...
A full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction ...
AbstractCompared with the one-dimensional trajectory correction technology which adjusts longitudina...
In some smart weapons, estimation of the impact point of the shell at each computation cycle of the ...
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spin...
The modified configuration of the 155 mm rocket assisted projectile equipped with lateral thrusters ...
In this paper, a new dual-spin guided projectile that is equipped with ten lateral impulse jets is p...
License, which permits unrestricted use, distribution, and reproduction in anymedium, provided the o...
The balance of stability and maneuverability is the foundation of the trajectory correction projecti...
The article presents the analysis of the impact point dispersion reduction using lateral correction ...
This paper presents a two-phase guidance and control algorithm to extend the range and improve the i...
Impact point model predictive control of a spin-stabilized projectile with instability protection Ma...
In external ballistics of a conventional spin-stabilised artillery projectile, there are a numberof ...
The launch and impact points of a flight trajectory are estimated using U-D Kalman filter and Rauch-...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical EngineeringThe ...
This paper presents an optimum control scheme of firing time and firing phase angle by taking impact...
A full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction ...
AbstractCompared with the one-dimensional trajectory correction technology which adjusts longitudina...
In some smart weapons, estimation of the impact point of the shell at each computation cycle of the ...
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spin...
The modified configuration of the 155 mm rocket assisted projectile equipped with lateral thrusters ...
In this paper, a new dual-spin guided projectile that is equipped with ten lateral impulse jets is p...
License, which permits unrestricted use, distribution, and reproduction in anymedium, provided the o...
The balance of stability and maneuverability is the foundation of the trajectory correction projecti...
The article presents the analysis of the impact point dispersion reduction using lateral correction ...
This paper presents a two-phase guidance and control algorithm to extend the range and improve the i...
Impact point model predictive control of a spin-stabilized projectile with instability protection Ma...
In external ballistics of a conventional spin-stabilised artillery projectile, there are a numberof ...
The launch and impact points of a flight trajectory are estimated using U-D Kalman filter and Rauch-...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical EngineeringThe ...
This paper presents an optimum control scheme of firing time and firing phase angle by taking impact...
A full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction ...