An overview on dynamics and controls modelling of hypersonic vehicles
Michael A. Bolender
- pp 2507-2512
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TLDR
This paper discusses the areas that are important to realizing a hypersonic modelling approach that can take any given vehicle geometry and permit a thorough analysis of its stability and control characteristics and any practical constraints on its operability, the design of a control law, an assessment of it closed-loop performance.Abstract:
In order to appropriately design control laws for hypersonic vehicles, it is paramount to understand how the flight dynamics are impacted by the interactions between the aerothermodynamics, propulsion system, structural dynamics, and control system. To this end, there has been a significant investment into the modelling of these sub-systems and their integration into a comprehensive model that can be used to the characterize the flight dynamics of scramjet-powered hypersonic aircraft and still remain amenable to control law design and analysis. In this paper, the development of a comprehensive model of the longitudinal dynamics of generic hypersonic vehicle with an outward-turning, two-dimensional inlet is described. The sub-system models, for the most part, are simple models derived from first-principles and are intended to capture the interactions between the different sub-systems to provide a representative vehicle model. We also will discuss the areas that are important to realizing a hypersonic modelling approach that can take any given vehicle geometry and permit a thorough analysis of its stability and control characteristics and any practical constraints on its operability, the design of a control law, an assessment of it closed-loop performance.read more
Citations
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Journal ArticleDOI
Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicle☆
TL;DR: In this article, a control-oriented uncertainty model is established for the feedback linearization design, and the multi-input and multi-output (MIMO) quasi-continuous high-order sliding mode (HOSM) controller is formulated to track the responses of the vehicle to a step change in velocity and altitude based on full state feedback.
Journal ArticleDOI
Continuous high order sliding mode controller design for a flexible air-breathing hypersonic vehicle.
TL;DR: An Input-Output linearization model is constructed for the purpose of feedback control design and a nonlinear disturbance observer is applied to estimate the uncertainties in order to compensate the controller and disturbance suppression, where disturbance observer and controller synthesis design is obtained.
Journal ArticleDOI
Adaptive high-order dynamic sliding mode control for a flexible air-breathing hypersonic vehicle
TL;DR: In this article, the problem of tracking control for a longitudinal air-breathing hypersonic vehicle model with flexible effects and intricate couplings between the engine dynamics and flight dynamics is investigated.
Journal ArticleDOI
Interval Type-2 FNN-Based Quantized Tracking Control for Hypersonic Flight Vehicles With Prescribed Performance
TL;DR: This paper presents a tracking control scheme with quantization mechanism for hypersonic flight vehicles (HFVs) with prescribed performance using an interval type-2 fuzzy neural network (IT2FNN).
Journal ArticleDOI
Immersion and Invariance-Based Output Feedback Control of Air-Breathing Hypersonic Vehicles
TL;DR: A new output feedback control design for robust velocity and altitude tracking of an air-breathing hypersonic vehicle (AHSV) is presented and the key idea is to employ the immersion and invariance approach to design globally asymptotically stable observers for the unmeasurable states.
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