Progress in Guidance and Control Research for Space Access and Hypersonic Vehicles

2006 ◽  
Author(s):  
David B. Doman ◽  
Michael W. Oppenheimer ◽  
Michael A. Bolender
Keyword(s):  
Hypersonic Vehicles ◽  
Guidance And Control ◽  
Control Research ◽  
And Control

Low-order diving integrated guidance and control for hypersonic vehicles

2019 ◽  
Vol 91 ◽  
pp. 96-109 ◽  
Author(s):  
JianHua Wang ◽  
Long Cheng ◽  
YuanWen Cai ◽  
GuoJian Tang
Keyword(s):  
Hypersonic Vehicles ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control ◽  
Low Order

scholarly journals A Low-Order Partial Integrated Guidance and Control Scheme for Diving Hypersonic Vehicles to Impact Ground Maneuver Target

2021 ◽  
Vol 2021 ◽  
pp. 1-12
Author(s):  
Tong An ◽  
JianHua Wang ◽  
YuLong Pan ◽  
HaiShan Chen
Keyword(s):  
Analytical Model ◽  
Sliding Mode ◽  
Design Method ◽  
Hypersonic Vehicle ◽  
Hypersonic Vehicles ◽  
Dynamic Surface ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control ◽  
Low Order

In this article, a low-order partial integrated guidance and control (PIGC) design method is proposed for diving hypersonic vehicles to impact ground maneuver target. A three-channel analytical model of body rates is deduced based on acceleration components of the hypersonic vehicle. By combining the analytical model of body rates and relative dynamic model between the hypersonic vehicle and target, three-channel commands of body rates are directly generated based on the extended state observer (ESO) technique, sliding mode control approach, and dynamic surface control theory in the guidance subsystem. In the attitude control subsystem, a sliding mode controller is designed to track the commands of body rates and generate commands of control surface fin deflections. By making full use of acceleration information of the hypersonic vehicle measured by the mounted accelerometer, the proposed PIGC design method provides a novel solution to compensate the unknown acceleration of the ground maneuver target. Besides, the order of design model is also reduced, and the design process is simplified. The effectiveness and robustness of the PIGC design method are verified and discussed by 6DOF simulation studies.

Adaptive Guidance and Control for Autonomous Hypersonic Vehicles

2006 ◽  
Vol 29 (3) ◽  
pp. 725-737 ◽  
Author(s):  
Eric N. Johnson ◽  
Anthony J. Calise ◽  
Michael D. Curry ◽  
Kenneth D. Mease ◽  
J. Eric Corban
Keyword(s):  
Hypersonic Vehicles ◽  
Guidance And Control ◽  
Adaptive Guidance ◽  
And Control

Guidance and Control Research on Underwater Unpowered Anti-Submarine Weapons

2013 ◽  
Vol 648 ◽  
pp. 323-327
Author(s):  
Jian Xiong
Keyword(s):  
Control Method ◽  
Control Model ◽  
Control Methods ◽  
Motion Model ◽  
Projectile Motion ◽  
Guidance And Control ◽  
Control Research ◽  
Double Plane ◽  
And Control ◽  
Control Trajectory

According to the underwater ballistic characteristics of unpowered anti-submarine weapon, double plane guidance of self-correcting ahead angle and tracing method was adopted. This paper established homing model, guidance, control model and the motion model of unpowered antisubmarine weapon. In typical combat situations, it carried out simulation about underwater guidance and control trajectory. Projectile motion properties were analyzed and it verified effectiveness of the guidance and control methods, it provided a basis for underwater trajectory planning, guidance and control method.

Finite-time integrated guidance and control system for hypersonic vehicles

2020 ◽  
pp. 014233122094193
Author(s):  
Chong Zhenyu ◽  
Guo Jianguo ◽  
Zhao Bin ◽  
Guo Zongyi ◽  
Lu Xiaodong
Keyword(s):  
Control System ◽  
Finite Time ◽  
Lyapunov Stability Theory ◽  
Hypersonic Vehicles ◽  
Nonlinear Simulation ◽  
Loop Control ◽  
Finite Time Stability ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control

A finite-time integrated guidance and control (IGC) method is proposed in this study for hypersonic vehicles. The IGC dynamic model is initially built by combining the 3D relative kinematics and dynamics equations. Then, by introducing the adaptive control technology and the backstepping approach, an IGC scheme with adaptive parameters is presented to guarantee the finite-time stability of a closed-loop control system on the basis of Lyapunov stability theory. Nonlinear simulation results demonstrate the effectiveness and robustness of the proposed IGC method for hypersonic vehicles compared with other robust IGC methods.

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