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检索条件"主题词=sequential gradient-restoration algorithm"
26 条 记 录,以下是1-10 订阅
Optimization and Analysis on Trajectory with Multiple Constraints for Hypersonic Air-vehicle
Optimization and Analysis on Trajectory with Multiple Constr...
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International Conference on Engineering Technology and Application (ICETA)
作者: Wei, Changzhu Huang, Rong Li, Hao Shan, Yongzhi Harbin Inst Technol Dept Aerosp Engn Sch Astronaut Harbin 150006 Heilongjiang Peoples R China Harbin Jiancheng Grp Co Ltd Harbin Heilongjiang Peoples R China
The trajectory optimization technology is one of the key technologies for hypersonic air-vehicle. There are multiple constraints in the process of hypersonic flight, such as uncertainty of flight environment, thermal ... 详细信息
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Optimization and Analysis on Trajectory with Multiple Constraints for Hypersonic Air-vehicle
Optimization and Analysis on Trajectory with Multiple Constr...
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The 2015 2nd International Conference on Engineering Technology and Application
作者: Changzhu Wei Rong Huang Hao Li Yongzhi Shan Department of Aerospace Engineering School of AstronauticsHarbin Institute of Technology Harbin Jiancheng Group Co.Ltd
The trajectory optimization technology is one of the key technologies for hypersonic *** are multiple constraints in the process of hypersonic flight,such as uncertainty of flight environment,thermal current,dynamic p... 详细信息
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Optimal starting conditions for the rendezvous maneuver, Part 2:: Mathematical programming approach
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JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 2008年 第3期137卷 625-639页
作者: Miele, A. Ciarcia, M. Rice Univ Aeroastronaut Grp Houston TX 77251 USA
In a companion paper (Part 1, J. Optim. Theory Appl. 137(3), 2008), we determined the optimal starting conditions for the rendezvous maneuver using an optimal control approach. In this paper, we study the same problem... 详细信息
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Optimal trajectories for spacecraft rendezvous
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JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 2007年 第3期132卷 353-376页
作者: Miele, A. Weeks, M. W. Ciarcia, M. Rice Univ Aeroastronaut Grp Houston TX 77251 USA NASA Lyndon B Johnson Space Ctr Aerosci & Flight Mech Div Houston TX 77058 USA
The efficient execution of a rendezvous maneuver is an essential component of various types of space missions. This work describes the formulation and numerical investigation of the thrust function required to minimiz... 详细信息
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Optimal dive recovery maneuvers of a supermaneuvering jet fighter aircraft
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JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS 2001年 第2-3期338卷 113-132页
作者: Miele, A Dabney, JB Rice Univ AeroAstronaut Grp Houston TX 77251 USA Univ Houston Dept Syst Engn Clear Lake TX USA
This paper describes an investigation of dive recovery maneuvers of a jet fighter aircraft capable of flying at angles of attack in the post-stall region. In a dive recovery maneuver, the pilot attempts to return the ... 详细信息
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Optimal control of a ship for course change and sidestep maneuvers
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JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1999年 第2期103卷 259-282页
作者: Miele, A Wang, T Chao, CS Dabney, JB Rice Univ Aero Astronaut Grp Houston TX 77251 USA Rice Univ Dept Mech Engn Houston TX 77251 USA
We consider a ship subject to kinematic, dynamic, and moment equations and steered via rudder under the assumptions that the rudder angle and rudder angle time rate are subject to upper and lower bounds. We formulate ... 详细信息
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Optimal control of a ship for collision avoidance maneuvers
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JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1999年 第3期103卷 495-519页
作者: Miele, A Wang, T Chao, CS Dabney, JB Rice Univ Aeroastronaut Grp Houston TX 77251 USA Rice Univ Dept Mech Engn Houston TX 77251 USA
We consider a ship subject to kinematic, dynamic, and moment equations and steered via rudder under the assumptions that the rudder angle and rudder angle time rate are subject to upper and lower bounds. We formulate ... 详细信息
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Optimal control of a ship for a course-changing maneuver
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JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1998年 第2期97卷 281-297页
作者: Tzeng, CY Natl Taiwan Ocean Univ Inst Maritime Technol Keelung Taiwan
The steering control of a ship during a course-changing maneuver is formulated as a Bolza optimal control problem, which is solved via the sequential gradient-restoration algorithm (SGRA). Nonlinear differential equat... 详细信息
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Optimal trajectories for Earth-to-Mars flight
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JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1997年 第3期95卷 467-499页
作者: Miele, A Wang, T Rice Univ Aeroastron Grp Houston TX 77251 USA
This paper deals with the optimal transfer of a spacecraft from a low Earth orbit (LEG) to a low Mars orbit (LMO). The transfer problem is formulated via a restricted four-body model in that the spacecraft is consider... 详细信息
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UTILIZING AN ENGINEERING OPTIMIZATION APPROACH TO PREDICT MAXIMUM MASS-FLOW RATES OF STEAM AND WATER MIXTURES
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ENGINEERING OPTIMIZATION 1995年 第4期23卷 267-285页
作者: LAM, TT [a] The Aerospace Corporation Los Angeles CA U.S.A
Two mass flux mathematical models for the study of critical single- and two-phase flows of water are formulated based on optimization theory. Analytical expressions for the mass flux functions are developed for the su... 详细信息
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