A roll-decoupled course correction fuze with canards can improve the hit accuracy of conventional unguided ammunitions. The fuze increases accuracy by reducing the effect of angular and translational motion produced by the cyclical yawing forces applied on the projectile. In order to investigate the influence of yawing forces on angular motion, a theoretical solution of the total yaw angle function with the cyclical yawing forces is deduced utilizing the 7 degrees of freedom (7-DOF) model designed for this calculation. Furthermore, a detailed simulation is carried out to determine the influence rules of yawing force on angular motion. The calculated results illustrate that, when the rotational speed of the forward part is close to the initi...
Phantom Yaw can be induced by e.g. small perturbations or deviations in geometry which cause an asym...
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spin...
This numerical study is about the alleviation of the Phantom Yaw Effect on a pitching missile. A pai...
AbstractA roll-decoupled course correction fuze with canards can improve the hit accuracy of convent...
License, which permits unrestricted use, distribution, and reproduction in anymedium, provided the o...
Abstract The present study investigates the epicyclic pitching and yawing motion phenomenon of spinn...
Generally, as a precision-guided weapon, the missile has many disadvantage such as high price, diffi...
Existing literature has shown that the control force at the nose could cause dynamic instability for...
The usual analysis of the steady state angular motion of a dynamically stable spinning missile assum...
An investigation has been made in the Langley high-speed 7- "by 10-foot tunnel to determine the...
The swerve response of fin- and spin-stabilized projectiles to control mechanism inputs is sometimes...
International audienceThis article explores in detail the influence of the sensor position on the pi...
An experimental program for the aerodynamic and flight dynamic characterization of current 5.56mm sm...
The paper considers the problem of angular orientation of anti-aircraft guns towards a moving air ta...
A reprint of the 63rd Aeroballistic Range Association Meeting, Brussels, Belgium, 1-4 October 2012. ...
Phantom Yaw can be induced by e.g. small perturbations or deviations in geometry which cause an asym...
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spin...
This numerical study is about the alleviation of the Phantom Yaw Effect on a pitching missile. A pai...
AbstractA roll-decoupled course correction fuze with canards can improve the hit accuracy of convent...
License, which permits unrestricted use, distribution, and reproduction in anymedium, provided the o...
Abstract The present study investigates the epicyclic pitching and yawing motion phenomenon of spinn...
Generally, as a precision-guided weapon, the missile has many disadvantage such as high price, diffi...
Existing literature has shown that the control force at the nose could cause dynamic instability for...
The usual analysis of the steady state angular motion of a dynamically stable spinning missile assum...
An investigation has been made in the Langley high-speed 7- "by 10-foot tunnel to determine the...
The swerve response of fin- and spin-stabilized projectiles to control mechanism inputs is sometimes...
International audienceThis article explores in detail the influence of the sensor position on the pi...
An experimental program for the aerodynamic and flight dynamic characterization of current 5.56mm sm...
The paper considers the problem of angular orientation of anti-aircraft guns towards a moving air ta...
A reprint of the 63rd Aeroballistic Range Association Meeting, Brussels, Belgium, 1-4 October 2012. ...
Phantom Yaw can be induced by e.g. small perturbations or deviations in geometry which cause an asym...
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spin...
This numerical study is about the alleviation of the Phantom Yaw Effect on a pitching missile. A pai...