The authors have been developing the guidance system of winged rocket using dynamically distributed genetic algorithm (DynDGA) for trajectory optimization. DynDGA is an advanced genetic algorithm (GA) which can enhance the variety of trajectories and maintain the trajectory search performance. However, DynDGA requires higher computing power. One of the simple solution for this problem is to reduce the number of individuals and generations, but it also degrades the solution search capability. For the implementation, authors need to make a tradeoff between these problems. Evolutionary algorithms (EAs) have proven successful in a vast number of static applications and the number of papers produced in this area is growing rapidly. However, they...
The minimization of operations and support resources of reusable launch vehicles is a complex task, ...
The main goal of this paper is to analyze different methodologies and to quantitatively compare a se...
The resource levels required for operation and support of reusable launch vehicles are typically def...
An algorithm based on the mechanics of natural genetics is used to solve two different optimization ...
The demand for increased payload or reduced propellant requirements requires the trajectories of spa...
The goal of trajectory planning is to shorten the flight distance as much as possible on the premise...
This paper describes an effort to optimize the design of an entire space launch vehicle to low-Earth...
This paper presents a novel evolutionary computation approach to three-dimensional path planning for...
AbstractFlight vehicle conceptual design appears to be a promising area for application of the Genet...
Spacecraft and space systems are complex and generally difficult to design. The computation for the ...
This paper describes a stochastic approach for comprehensive diagnostics and validation of control s...
Evolutionary algorithms (EA) are a computation tool that utilizes biological principles found in th...
The development of new mission concepts requires efficient methodologies to analyze, de-sign, and si...
ABSTRACT: For a given set of celestial bodies, the problem of finding an optimal sequence of gravity...
This paper addresses the path planning problem of multiple unmanned aerial vehicles (UAVs). The path...
The minimization of operations and support resources of reusable launch vehicles is a complex task, ...
The main goal of this paper is to analyze different methodologies and to quantitatively compare a se...
The resource levels required for operation and support of reusable launch vehicles are typically def...
An algorithm based on the mechanics of natural genetics is used to solve two different optimization ...
The demand for increased payload or reduced propellant requirements requires the trajectories of spa...
The goal of trajectory planning is to shorten the flight distance as much as possible on the premise...
This paper describes an effort to optimize the design of an entire space launch vehicle to low-Earth...
This paper presents a novel evolutionary computation approach to three-dimensional path planning for...
AbstractFlight vehicle conceptual design appears to be a promising area for application of the Genet...
Spacecraft and space systems are complex and generally difficult to design. The computation for the ...
This paper describes a stochastic approach for comprehensive diagnostics and validation of control s...
Evolutionary algorithms (EA) are a computation tool that utilizes biological principles found in th...
The development of new mission concepts requires efficient methodologies to analyze, de-sign, and si...
ABSTRACT: For a given set of celestial bodies, the problem of finding an optimal sequence of gravity...
This paper addresses the path planning problem of multiple unmanned aerial vehicles (UAVs). The path...
The minimization of operations and support resources of reusable launch vehicles is a complex task, ...
The main goal of this paper is to analyze different methodologies and to quantitatively compare a se...
The resource levels required for operation and support of reusable launch vehicles are typically def...