Three-Dimensional Diving Guidance for Hypersonic Gliding Vehicle via Integrated Design of FTNDO and AMSTSMC

Liao, Yuxin; Li, Huifeng; Bao, Weimin

doi:10.1109/tie.2017.2736499

Cited by 29 publications

(9 citation statements)

References 33 publications

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“…Remark 3. As in many literatures, the angle constraints can be transformed to be LOS angle constraints [17][18][19][20][21][22][23][24]. The proposed LOS angle constrained guidance law shows the feasibility of the presented HP guidance design framework.…”

Section: Ntsm Based Angle Constrained Guidancementioning

confidence: 87%

“…Furthermore, the LOS angle constrained finite-time robust HP guidance problem can also be addressed based on the new nominal model. In many literature, angle constraints are usually transformed to be the LOS angle constraints, such as field-of-view constrained problems [17,18] and impact angle constrained problems [19][20][21][22][23][24]. Due to the axial symmetry property between the missile-based LOS coordinate system and the target-based LOS coordinate system, the LOS angle constraints for the interceptor missile can be easily transformed to be the constraints of the target's LOS angle.…”

Section: Introductionmentioning

confidence: 99%

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Robust Head-Pursuit Guidance Accounting for Hit-to-Kill and Angle Constraints

2021

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In this paper, the hit-to-kill strategy is introduced to solve the three-dimensional (3D) robust head-pursuit (HP) interception problem considering the line-of-sight (LOS) angle constraints. Firstly, a target based relative dynamic model is proposed to be the nominal model for designing the robust HP guidance laws, where the HP interception problem is formulated as a target passively chases after the interceptor missile. Secondly, the 3D retro-proportional navigation (RPN) guidance law is reinterpreted from the point of control theory, which forces the corresponding guidance system asymptotically stable. Meanwhile, the concept of nullifying the LOS angular rates is successfully introduced to solve the 3D robust HP guidance problem via the sliding mode control. Thirdly, the LOS angles constrained robust HP guidance law is proposed based on the nonsingular terminal sliding mode control. The stabilities of the presented guidance laws are analyzed via the Lyapunov approach. The simulation results are in agreement with the theoretical statements.

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Section: Ntsm Based Angle Constrained Guidancementioning

confidence: 87%

Section: Introductionmentioning

confidence: 99%

Robust Head-Pursuit Guidance Accounting for Hit-to-Kill and Angle Constraints

2021

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“…(21)- (23). From (22), we can also obtain a relation of the same form as (7) which has the specific form…”

Section: Performance Analysismentioning

confidence: 99%

“…Later, through the results in [20], a new reduced-order multiple observer was developed in [21] to achieve the finite-time r econstruction of the system's states associated with T-S multiple models. In addition, DOB techniques have been applied widely to many practical applications, such as the guidance law design for a hypersonic gliding vehicle [22], the attitude control of a spacecraft [23], and the direct yaw-moment control of an electric vehicle [24].…”

Section: Introductionmentioning

confidence: 99%

Disturbance Observer Design for Nonlinear Systems Represented by Input–Output Models

Ding

Chen

Mei

et al. 2020

IEEE Trans. Ind. Electron.

221

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A new approach to the design of nonlinear disturbance observers for a class of nonlinear systems described by inputoutput differential equations is presented in this paper. In contrast with established forms of nonlinear disturbance observers, the most important feature of this new type of disturbance observer is that only measurement of the output variable is required, rather than the state variables. An inverse simulation model is first constructed based on knowledge of the structure and parameters of a conventional model of the system. The disturbance can then be estimated by comparing the output of the inverse model and the input of the original nonlinear system. Mathematical analysis demonstrates the convergence of this new form of nonlinear disturbance observer. The approach has been applied to disturbance estimation for a linear system and a new form of linear disturbance observer has been developed. The differences between the proposed linear disturbance observer and the conventional form of frequency-domain disturbance observer are discussed through a numerical example. Finally, the nonlinear disturbance observer design method is illustrated through an application involving a simulation of a jacketed continuous stirred tank reactor system.

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“…In [23], a new model predictive convex programming was proposed for state and input constrained vehicle guidance design and a convex optimization framework was defined considering a flexibly designed cost function. In [24], a three-dimensional multiple constrained guidance problem for a hypersonic gliding vehicle (HGV) against a stationary ground target in the dive phase was investigated. In [25], a twisting control-based guidance law considering nonlinear/coupled dynamics and terminal angle constraints was proposed.…”

Section: Introductionmentioning

confidence: 99%