A new cooperative guidance law based on terminal sliding mode with strengthened condition is designed to solve multi-attacker-one-target simultaneous attack problem.The strengthened condition can guarantee state convergency and eliminate chattering.Accurate time-to-go can be kept during state moving on the sliding mode.The impact time can be given before intercepting target.Numerical simulations with the comparisons demonstrate the effectiveness and the superiority of the proposed cooperative guidance law.A new cooperative guidance law based on terminal sliding mode with strengthened condition is designed to solve multi-attacker-one-target simultaneous attack problem.The strengthened condition can guarantee state convergency and eliminate c...
Cooperative guidance is an important research direction in the field of missile guidance in recent y...
When threatened by a pursuer, an evading aircraft launches two defenders to accomplish a cooperative...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
In this paper,a new time-varying terminal sliding mode with unknown uncertainty bounds is designed t...
In order to realize a saturation attack of multiple unmanned aerial vehicles (UAVs) on the same targ...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
In this paper, a new time-varying terminal sliding mode with unknown uncertainty bounds is designed ...
In this paper, a new time-varying terminal sliding mode with unknown uncertainty bounds is designed ...
In this paper, a new dynamic surrounding attack cooperative guidance law against highly maneuvering ...
A cooperative attack problem with field-of-view constraint is considered for the nonlinear model of ...
Aiming at the problem of limited field-of-view of air-to-air missile during cooperative attack, a co...
A cooperative attack problem with field-of-view constraint is considered for the nonlinear model of ...
In this paper, a new cooperative guidance scheme is proposed capable of driving N number of missiles...
Aimed at the poor performance of guidance algorithms designed based on a linearized model in active ...
Cooperative guidance is an important research direction in the field of missile guidance in recent y...
When threatened by a pursuer, an evading aircraft launches two defenders to accomplish a cooperative...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
In this paper,a new time-varying terminal sliding mode with unknown uncertainty bounds is designed t...
In order to realize a saturation attack of multiple unmanned aerial vehicles (UAVs) on the same targ...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
In this paper, a new time-varying terminal sliding mode with unknown uncertainty bounds is designed ...
In this paper, a new time-varying terminal sliding mode with unknown uncertainty bounds is designed ...
In this paper, a new dynamic surrounding attack cooperative guidance law against highly maneuvering ...
A cooperative attack problem with field-of-view constraint is considered for the nonlinear model of ...
Aiming at the problem of limited field-of-view of air-to-air missile during cooperative attack, a co...
A cooperative attack problem with field-of-view constraint is considered for the nonlinear model of ...
In this paper, a new cooperative guidance scheme is proposed capable of driving N number of missiles...
Aimed at the poor performance of guidance algorithms designed based on a linearized model in active ...
Cooperative guidance is an important research direction in the field of missile guidance in recent y...
When threatened by a pursuer, an evading aircraft launches two defenders to accomplish a cooperative...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...