■ View full text

IEEE Transactions on Aerospace and Electronic Systems

https://ieeexplore.ieee.org/abstract/document/6494416

■ Researchers

Chang-Hun Lee

Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST)

C. H. Lee*, M. J. Tahk, and J. I. Lee

■ Abstract

The generalized formulation of weighted optimal guidance laws with impact angle constraint is investigated here. From the generalized formulation, we explicitly find the feasible set of weighting functions that lead to analytical forms of weighted optimal guidance laws. This result has potential significance because it can provide additional degrees of freedom in designing a guidance law that accomplishes the specified guidance objective.

• Acceleration
• Cost function
• Optimal control
• Missiles , Kinematics
• Equations

• [신진연구자] 항공우주시스템의 유도제어 알고리즘 연구