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Haizhao Liang, Haodong Yang, Jingxian Zhu, Jianying Wang
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Impact angle and impact velocity constrained terminal guidance for stationary target
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2003
Analytical time-coordinated entry guidance for multi-hypersonic vehicles within three-dimensional corridor
10.1016/j.ast.2024.109639 · doi-reference
Impact angle and impact velocity constrained terminal guidance for stationary target
10.1108/aeat-09-2013-0164 · doi-reference
Three-dimensional geometric descent guidance with impact angle constraint
10.1109/access.2020.2984353 · doi-reference
Optimization of multi-target continuous dynamic trajectory for unmanned aerial vehicles
10.1016/j.ast.2024.108958 · doi-reference
A model predictive solution to cooperative guidance of hypersonic reentry vehicle with impact angle and distance coordination
10.1016/j.ast.2023.108855 · doi-reference
Reduced-order entry trajectory planning for acceleration guidance
10.2514/2.4906 · doi-reference
Cooperative guidance strategy for multiple hypersonic gliding vehicles system
10.1016/j.cja.2019.12.003 · doi-reference
Adaptive entry guidance with time and full state constraints using analytical drag-vs-energy profile
10.1016/j.asr.2025.04.017 · doi-reference
Rapid and near-analytical planning method for entry trajectory under time and full-state constraints
10.3390/aerospace11070580 · doi-reference
Entry guidance with terminal approach angle constraint
10.1016/j.ast.2020.105876 · doi-reference
Waypoint constrained guidance for entry vehicles
10.1016/j.ast.2016.02.023 · doi-reference
An adaptive re-entry spatial-temporal cooperative guidance method under optimal topology
10.1155/ijae/2636385 · doi-reference
Analytical cooperative entry guidance for rendezvous and formation flight
10.1016/j.actaastro.2020.02.044 · doi-reference
Entry trajectory planning with terminal full states constraints and multiple geographic constraints
10.1016/j.ast.2018.10.035 · doi-reference
Lateral entry guidance with terminal time constraint
10.1109/taes.2022.3215554 · doi-reference
Time-coordination entry guidance using a range-determined strategy
10.1016/j.ast.2022.107842 · doi-reference
Time-coordination entry guidance for multi-hypersonic vehicles
10.1016/j.ast.2019.03.056 · doi-reference
Analytical entry guidance for coordinated flight with multiple no-fly-zone constraints
10.1016/j.ast.2018.10.013 · doi-reference
Analytic time reentry cooperative guidance for multi-hypersonic glide vehicles
10.3390/app13084987 · doi-reference
Entry guidance with terminal time control based on quasi-equilibrium glide condition
10.1109/taes.2019.2921213 · doi-reference
Predictor-corrector reentry guidance for hypersonic glide vehicles based on high-precision analytical solutions
10.1016/j.ast.2024.109545 · doi-reference
Constrained predictor-corrector guidance via bank saturation avoidance for low L/D entry vehicles
10.1016/j.ast.2020.106448 · doi-reference
Predictor-corrector entry guidance with waypoint and no-fly zone constraints
10.1016/j.actaastro.2017.05.009 · doi-reference
A hybrid discretization strategy for successive convex programming in skip entry trajectory optimization
10.1016/j.ast.2025.110056 · doi-reference
A novel re-entry trajectory design strategy enforcing inequality and terminal constraints in height-velocity plane
10.1016/j.asr.2023.12.013 · doi-reference
Multitask-constrained reentry trajectory planning for hypersonic gliding vehicle
10.1016/j.ast.2024.109636 · doi-reference
Entry trajectory optimization with general polygonal no-fly zone constraints
10.1109/taes.2023.3319590 · doi-reference
An enlarged polygon method without binary variables for obstacle avoidance trajectory optimization
10.1016/j.cja.2023.03.053 · doi-reference
Weight-adaptive parameter estimation assisted event-triggered model predictive guidance for reentry
10.1016/j.ast.2025.109938 · doi-reference
Geometric approach to lateral guidance for reentry vehicle
10.1109/taes.2024.3449247 · doi-reference
Analytical reentry guidance framework based on swarm intelligence optimization and altitude-energy profile
10.1016/j.cja.2023.07.029 · doi-reference
Highly constrained entry trajectory generation
10.1016/j.actaastro.2013.01.024 · doi-reference