In this paper the cubic spline guidance law is presented for intercepting a stationary target at a desired impact angle. The guidance law is obtained from cubic spline curve\ud based trajectory using an inverse method. The cubic spline t\ud rajectory curve expresses the altitude as a cubic polynomial of the downrange. The guidance law is modified to achieve interception in the cases where impact angle is greater that or equal to 90◦. The guidance law is implemented in a feedback mode to maintain the desired\ud impact angle and to reduce miss distance in the presence of lateral acceleration saturation and atmospheric distur- bances. The simulation results show that the guidance law fulfills all the requirements
Impact angle constrained guidance laws are important in many applications such as guidance of torped...
Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach Yao ...
This Correspondence proposes a new guidance law based on integral sliding mode control (ISMC) techni...
In this paper, a cubic spline guidance law is proposed for intercepting a stationary target at a des...
In this thesis the cubic spline guidance law and its variants are derived. A detailed analysis is c...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
Impact angle controlled interception of stationary targets is considered in a surface-to-surface eng...
This paper presents an impact-angle-control guidance law with terminal constraints on the curvature ...
In Many advanced guidance applications [1–5], it is required to intercept the target from a particul...
A polynomial based guidance law dependent on range-to-go, is proposed for interception of a non-mane...
An optimal impact angle control guidance law is proposed in this paper.The missile system is approxi...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...
This paper presents an intercept angle guidance law against moving targets in an environment with se...
In the guidance literature, minimizing miss distance along with optimizing the energy usage had been...
Impact angle constrained guidance laws are important in many applications such as guidance of torped...
Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach Yao ...
This Correspondence proposes a new guidance law based on integral sliding mode control (ISMC) techni...
In this paper, a cubic spline guidance law is proposed for intercepting a stationary target at a des...
In this thesis the cubic spline guidance law and its variants are derived. A detailed analysis is c...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
Impact angle controlled interception of stationary targets is considered in a surface-to-surface eng...
This paper presents an impact-angle-control guidance law with terminal constraints on the curvature ...
In Many advanced guidance applications [1–5], it is required to intercept the target from a particul...
A polynomial based guidance law dependent on range-to-go, is proposed for interception of a non-mane...
An optimal impact angle control guidance law is proposed in this paper.The missile system is approxi...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...
This paper presents an intercept angle guidance law against moving targets in an environment with se...
In the guidance literature, minimizing miss distance along with optimizing the energy usage had been...
Impact angle constrained guidance laws are important in many applications such as guidance of torped...
Terminal impact angle constrained guidance laws using state-dependent Riccati equation approach Yao ...
This Correspondence proposes a new guidance law based on integral sliding mode control (ISMC) techni...