Add to ORKGThis paper explores the various analytical links between the free attitude motions of spinning bodies of the rocket type, and the system's parameters. The system is modeled as an axisymmetric body with substantial mass loss, and special attention is paid to the presence of a nozzle on the system. It is found that the nozzle expansion ratio can have an important influence on attitude motion, the higher this ratio the better behaved the system
Two 10-inch-diameter spherical rocket motors have been flight tested at the NASA Wallops Station. Th...
Abstract:- This work involves the research of a motion of a mechanical system consisting from coaxia...
The attitude motion of a spin-stabilized, upper-stage spacecraft is investigated based on a two-body...
In classical mechanics, the ‘geometry of motion’ refers to a development to visualize the motion of ...
This paper examines the rotational motion of a nearly axisymmetric rocket type system with uniform b...
This paper evaluates the impact that helical motion of fluid products of combustion within the combu...
A theoretical study was conducted to determine the motion of nonstabilized rolling and spinning bodi...
The objective of this research is to develope analytical solutions for the translational and rotatio...
The attitude dynamics and manoeuvre survey in this paper is performed for a mission scenario involvi...
During axial thrusting of a spin-stabilized spacecraft undergoing orbital injections or control mane...
The usual analysis of the steady state angular motion of a dynamically stable spinning missile assum...
Abstract--For p oblems involving rotating rigid bodies (e.g. spin-stabilized satellites inspace) one...
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
Spinning a ballistic missile is a common practice to stabilize the attitude of the vehicle; however,...
This paper demonstrates a guidance and control scheme for a spinning, aerodynamically asymmetrical v...
Two 10-inch-diameter spherical rocket motors have been flight tested at the NASA Wallops Station. Th...
Abstract:- This work involves the research of a motion of a mechanical system consisting from coaxia...
The attitude motion of a spin-stabilized, upper-stage spacecraft is investigated based on a two-body...
In classical mechanics, the ‘geometry of motion’ refers to a development to visualize the motion of ...
This paper examines the rotational motion of a nearly axisymmetric rocket type system with uniform b...
This paper evaluates the impact that helical motion of fluid products of combustion within the combu...
A theoretical study was conducted to determine the motion of nonstabilized rolling and spinning bodi...
The objective of this research is to develope analytical solutions for the translational and rotatio...
The attitude dynamics and manoeuvre survey in this paper is performed for a mission scenario involvi...
During axial thrusting of a spin-stabilized spacecraft undergoing orbital injections or control mane...
The usual analysis of the steady state angular motion of a dynamically stable spinning missile assum...
Abstract--For p oblems involving rotating rigid bodies (e.g. spin-stabilized satellites inspace) one...
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
Spinning a ballistic missile is a common practice to stabilize the attitude of the vehicle; however,...
This paper demonstrates a guidance and control scheme for a spinning, aerodynamically asymmetrical v...
Two 10-inch-diameter spherical rocket motors have been flight tested at the NASA Wallops Station. Th...
Abstract:- This work involves the research of a motion of a mechanical system consisting from coaxia...
The attitude motion of a spin-stabilized, upper-stage spacecraft is investigated based on a two-body...