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Longitudinal stability and control characteristics at a Mach number of 2.01 of several simulated air-launched ballistic missiles having various types of control surfaces

机译：具有各种控制面的几种模拟空射弹道导弹的马赫数为2.01时的纵向稳定性和控制特性

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作者
Robinson, R. B.; Spearman, M. L.;
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年度 1961
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BALLISTIC MISSILES; CONTROL SURFACES; LONGITUDINAL STABILITY; AERODYNAMIC CHARACTERISTICS; COMPUTERIZED SIMULATION; SUPERSONIC SPEED; WIND TUNNEL STABILITY TESTS;

机译：BaLLIsTIC mIssILEs;控制表面;纵向稳定性;空气动力学特征;计算机模拟;超音速;风洞稳定性试验;

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1. Robust Hybrid Control for Ballistic Missile Longitudinal Autopilot [J] . WAEL Mohsen Ahmed, QUAN Quana 中国航空学报（英文版） . 2011,第006期

机译：弹道导弹纵向自动驾驶的鲁棒混合控制。
2. Kinzhal air-launched ballistic missile [J] . Rahul Udoshi Jane's Defence Weekly . 2019,第43期

机译：金扎尔空射弹道导弹
3. ISRAEL HAS DEVELOPED AN AIR-LAUNCHED BALLISTIC MISSILE [J] . DAVID AXE Combat Aircraft Monthly . 2018,第9期

机译：以色列开发了一个空气发射的弹道导弹
4. CONTROLLING BALLISTIC MISSILE DEFENSE AND ANTI-SATELLITE MISSILES: SHOULD WE LOOK ELSEWHERE OR RATHER AMEND ART. IV OST? [C] . Abhyudaya Agarwal, Kaushika Vuppala, Ramanuj Mukherjee International astronautical congress;IAC 2008 . 2008

机译：控制弹道导弹防御和反卫星导弹：我们应该在其他地方查找或修改艺术品。 IV OST？
5. PROJECT MANAGEMENT VERSUS FUNCTIONAL MANAGEMENT: A CASE STUDY OF THE FLEET BALLISTIC MISSILE, THE SURFACE MISSILE SYSTEMS AND THE INSHORE WARFARE PROJECTS AND THEIR SUPPLY SUPPORT RELATIONSHIPS WITH THE NAVAL SUPPLY SYSTEMS COMMAND [D] . STALEY, SAMUEL SORBER, III. 1971

机译：项目管理与功能管理：以舰队弹道导弹，地面导弹系统和室内武器项目为例的研究及其与海军供应系统的供应支持关系
6. Microencapsulation of immunoglobulin Y: optimization with response surface morphology and controlled release during simulated gastrointestinal digestion [O] . Jin Zhang, Huan-huan Li, Yi-fan Chen, 2020

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7. Robust Hybrid Control for Ballistic Missile Longitudinal Autopilot [O] . WAEL Mohsen Ahmed, QUAN Quan 2011

机译：弹道导弹纵向自动驾驶的鲁棒混合控制。
8. Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces [R] . Foster, G. V., Robinson, R. B. 1961

机译：具有全可动翼和尾表面的高超音速导弹配置的机械数为2.01的静态纵向稳定性和控制特性

Longitudinal stability and control characteristics at a Mach number of 2.01 of several simulated air-launched ballistic missiles having various types of control surfaces

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