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Nonsingular continuous finite-time convergent guidance law with impact angle constraints
Luyao Zang
*
,
Defu Lin
, Yi Ji
*
Corresponding author for this work
School of Aerospace Engineering
Beijing Institute of Technology
Research output
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Contribution to journal
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Article
›
peer-review
6
Citations (Scopus)
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Engineering
Boundedness
25%
Computer Simulation
25%
Convergent
100%
Demonstrates
25%
Finite Time
100%
Impact Angle
100%
Second-Order Sliding-Mode Control
25%
Singularities
25%
Sliding Mode
75%
Target Manoeuvre
25%