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missile
On the development of future missile complexes for strategic nuclear forces
      
Possibilities of defense from a missile attacking from the back hemisphere by a vertical maneuver
      
The possibilities to defend an aircraft attacked from the back hemisphere by an air-air missile are investigated.
      
A model problem of determining an optimal vertical maneuver of the aircraft evading a missile that moves in the exponential atmosphere according to a given law of approach subject to aerodynamic drag forces and the Earth's gravitation is studied.
      
With a delay caused by the fact that the missile-flight time is finite, these distributions contain passive zones (i.e., time intervals where shooting makes no sense).
      
Optimal instants for missile launching missiles and application of jamming in a duel situation of fighters
      
Variable centroid control scheme over hypersonic tactical missile
      
This paper presents a brand-new tactical missile control scheme-variable centroid vector control according to the international highlight in the field of missile control and the research status of hypersonic missile control in China.
      
The network has mixed traffic, one type of packet needs an Acknowledgement(Ack), the other type does not need, the background of such a network is tactical missile systems.
      
These detectors have been integrated successfully into many different types of system including missile seekers, time delay integration scanning systems, hand-held cameras, missile warning systems and many others.
      
The implications of the chemical war threat and the missile attacks during the Gulf War for a medium-sized psychiatric community are analyzed in terms of psychiatric care and management.
      
This includes damage not directly attributable to the missile itself, in other words, that due to cavitation.
      
Sliding mode control for an aerodynamic missile based on backstepping design
      
The SMC based on the backstepping design is applied to the flight control system design of an aerodynamic missile.
      
The results demonstrate that the designed controller yields a fast responding system, and the resulting DG guidance and control system is viable and effective in a realistic missile defense engagement.
      
As the residue of temporary cavity formation, mantle-like hemorrhagic destruction zones were seen surrounding the missile track that showed an eccentric, conical extension enlarging toward subpleural lung segments.
      
Potential effects, however, can be garnered by studying the medical effects of other acute stressors, such as earthquakes, missile attacks, and the like.
      
Development of guidance laws for a variable-speed missile
      
Indeed, if a missile and a target move on a collision course with constant speeds, the LOS rate is zero.
      
The speed of a highly maneuverable modem missile varies considerably during flight.
      
 

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