ETRI-Knowledge Sharing Plaform

KOREAN
논문 검색
Type SCI
Year ~ Keyword

Detail

Journal Article Real-Time Terrain-Following Guidance for Mitigation of Pilot-Induced Oscillations
Cited - time in scopus Share share facebook twitter linkedin kakaostory
Authors
Kwangwoo Jang, Youngjae Kim, Sukjae Im, Man Jun Koh, Hyochoong Bang
Citation
Journal of Guidance, Control, and Dynamics, pp.1-17
ISSN
0731-5090
Publisher
American Institute of Aeronautics and Astronautics
Language
English
Type
Journal Article
DOI
https://dx.doi.org/10.2514/1.G009574
Abstract
Terrain-following (TF) guidance is essential for evading radar detection and enabling safe low-altitude flight. While optimal-control-based TF methods have addressed terrain constraints, they remain limited by computational complexity, input saturation, and pilot-induced oscillations (PIOs). PIOs are particularly hazardous, as they induce sustained oscillations that can cause excessive overshoot over high terrain or collisions. This paper presents a real-time guidance framework that embeds a human pilot model into a model predictive path integral (MPPI) controller with terrain-dependent weighted cost functions. A path-integral-based parameter estimation (PIPE) algorithm is developed to adaptively identify pilot gain and delay online, enabling in-flight suppression of PIOs. Simulation results demonstrate that the proposed MPPI–PIPE framework reduces terrain-following oscillation amplitude by 36.8% compared to MPPI without pilot adaptation, while maintaining real-time feasibility through GPU-parallelized trajectory sampling. Hardware-in-the-loop simulation results further confirm effective PIO mitigation and accurate low-altitude tracking across diverse pilot characteristics.
Keyword
Pilot Induced Oscillation, Aerospace Engineering, Optimal Control Problem, Radar Detection, Hardware in the Loop SimulationModel Reference Adaptive ControlFlight Control SurfacesAircraft Flight Control SystemMilitary TechnologyHeight Above Ground Level
KSP Keywords
Aerospace engineering, Computational complexity, Cost Function, Hardware-in-The-loop simulation, In-flight, Induced oscillations, Model predictive, Parameter estimation, Path integral, Pilot model, Real-time guidance