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Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints

机译：具有姿态和姿态速率约束的最优三维运载火箭轨迹

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摘要

Mathematical models for optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints

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作者
Spurlock, O. F.; Teren, F.;
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作者单位

展开▼
年度 1969
页码 1-49
总页数 49
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LAUNCH VEHICLES; MATHEMATICAL MODELS; THREE DIMENSIONAL MOTION; CALCULUS OF VARIATIONS; DIFFERENTIAL EQUATIONS; EQUATIONS OF MOTION; PAYLOADS; TRAJECTORY ANALYSIS; WEIERSTRASS FUNCTIONS;

机译：发射车辆;数学模型;三维运动;变化的计算;微分方程;运动方程;有效载荷;轨迹分析; WEIERsTRass函数;

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专利

1. Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase [J] . Tian B., Fan W., Su R., Industrial Electronics, IEEE Transactions on . 2015,第3期

机译：再入阶段可重复使用运载火箭的实时轨迹和姿态协调控制
2. Perceived benefits and constraints in vehicle automation: Data to assess the relationship between driver's features and their attitudes towards autonomous vehicles [J] . Ignacio Lijarcio, Sergio A. Useche, Javier Llamazares, Data in Brief . 2019,第2期

机译：汽车自动化的感知效益和限制：评估驾驶员特征与对自动车辆态度之间关系的数据
3. Attitude control of reusable launch vehicle in reentry phase with input constraint via robust adaptive backstepping control [J] . Wang Fang, Hua Changchun, Zong Qun International Journal of Adaptive Control and Signal Processing . 2015,第10期

机译：具有鲁棒自适应反推控制的具有输入约束的可重用运载火箭进入再入阶段的姿态控制
4. Trajectory optimization and adaptive fuzzy based Launch Vehicle attitude control [C] . Ansari Uzair, Alam Saqib, Jafri Syed Minhaj un Nabi 2012 20th Mediterranean Conference on Control amp; Automation . 2012

机译：基于轨迹优化和自适应模糊的运载火箭姿态控制
5. Optimal trajectory designs and systems engineering analyses of reusable launch vehicles. [D] . Tsai, Hung-i Bruce. 2003

机译：可重复使用运载火箭的最佳轨迹设计和系统工程分析。
6. Perceived benefits and constraints in vehicle automation: Data to assess the relationship between drivers features and their attitudes towards autonomous vehicles [O] . Ignacio Lijarcio, Sergio A. Useche, Javier Llamazares, 2019

机译：车辆自动化的感知优势和局限性：评估驾驶员特征与其对自动驾驶态度之间关系的数据
7. Trajectory and Attitude Analysis for the 1st Flight Test of KSLV-I Launch Vehicle [O] . Woong-Rae Roh, Sang-Bum Cho, Jeong-Hwan Ko, 2010

机译：KSLV-I发射车辆第一飞行试验的轨迹和态度分析

Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints

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