The problem of intercepting a maneuvering target at a prespecified impact angle is posed in nonlinear zero-sum differential games framework. A feedback form solution is proposed by extending state-dependent Riccati equation method to nonlinear zero-sum differential games. An analytic solution is obtained for the state-dependent Riccati equation corresponding to the impact-angle-constrained guidance problem. The impact-angle-constrained guidance law is derived using the states line-of-sight rate and projected terminal impact angle error. Local asymptotic stability conditions for the closed-loop system corresponding to these states are studied. Time-to-go estimation is not explicitly required to derive and implement the proposed guidance law....
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
New developments and improvements on evasive missiles have led to a situation in which the current m...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...
A guidance law derived by modifying state dependent Riccati equation technique, to enable the imposi...
State-dependent Riccati equation (SDRE) techniques are rapidly emerging as general design methods fo...
In this report the application of the differential game theory to missile guidance problem is consid...
The guidance problem of a confrontation between an interceptor, a hypersonic vehicle, and an active ...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach Yao ...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
This thesis addresses several aerospace guidance and decision making problems using both no cooperat...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
This paper discusses the problem of impact time control of an interceptor against a stationary targe...
This paper discusses the problem of impact time control of an interceptor against a stationary targe...
A differential game based cooperative guidance strategy is proposed for the active-aircraft defence ...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
New developments and improvements on evasive missiles have led to a situation in which the current m...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...
A guidance law derived by modifying state dependent Riccati equation technique, to enable the imposi...
State-dependent Riccati equation (SDRE) techniques are rapidly emerging as general design methods fo...
In this report the application of the differential game theory to missile guidance problem is consid...
The guidance problem of a confrontation between an interceptor, a hypersonic vehicle, and an active ...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach Yao ...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
This thesis addresses several aerospace guidance and decision making problems using both no cooperat...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
This paper discusses the problem of impact time control of an interceptor against a stationary targe...
This paper discusses the problem of impact time control of an interceptor against a stationary targe...
A differential game based cooperative guidance strategy is proposed for the active-aircraft defence ...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
New developments and improvements on evasive missiles have led to a situation in which the current m...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...