Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint
By Tae-Hun Kim, Bong-Gyun Park, Min-Jae Tahk. 2013
180 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Statistical and Nonlinear Physics
View Paper: https://www.semanticscholar.org/paper/d0b2c0adf80086bf9201551a86df2434cc34eefe
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- Rajarshi Bardhan
- Raziye Tekin
- Koray S. Erer
- Debasish Ghose
- Tae-Hun Kim
- Bong-Gyun Park
- Hyuck-Hoon Kwon
- Yoon-Hwan Kim
In Statistical and Nonlinear Physics
- Rajarshi Bardhan
- Raziye Tekin
- Koray S. Erer
- Debasish Ghose
- Tae-Hun Kim
- Hyuck-Hoon Kwon
- Yoon-Hwan Kim
- Bong-Gyun Park
Citations in the corpus
- Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “Two-phase guidancescheme-based biased proportional navigation guidance laws were proposed in [5,6] for impact-angle control against stationary targets.”
- Composite Guidance Scheme for Impact Angle Control Against a Nonmaneuvering Moving Target (2016, methodology): “[11] proposed a biasshaping method, based on the work in [7], to consider the look-angle and acceleration limits.”
- Switched-Gain Guidance for Impact Angle Control Under Physical Constraints (2015, methodology): “Also, the guidance law of [26] is able to deal with the acceleration constraint onlywhen the LOS rate is negligible, which is likely to constitute certain difficulties as the engagement nears its end.”