This paper deals with the large Angle attitude maneuver control of spacecrafts.
本文研究空间飞行器大角度姿态机动的控制问题。
The rapid speed attitude maneuver based on SGCMG for small satellite is also studied.
研究了使用SGCMG的航天器的快速姿态机动问题。
In this paper, the issue on fast attitude maneuver control of a spacecraft with flexible appendix is studied.
研究带柔性附件航天器的姿态快速机动控制问题。
Pre-planning method based on state-space search for attitude maneuver un-der complex constraints was studied.
研究了基于状态空间搜索的复杂约束姿态机动预先规划方法。
The attitude stabilization, attitude maneuver, and attitude track for the reconfigurable spacecrafts are studied.
研究了姿态稳定、姿态机动和姿态跟踪问题。
This article investigates the spacecraft autonomous attitude maneuver control in the presence of forbidden attitude.
主要研究存在禁止姿态的航天器自主姿态机动控制问题。
The research results show that the modified guidance law can meet the need of pinpoint soft landing using the achievable attitude maneuver capability.
研究结果表明，利用一定的姿态机动能力，修正的制导方法能够满足精确软着陆的需要。
To solve the attitude maneuver of a flexible satellite, this article presents a variable structure tracking control algorithm based on output feedback.
为解决柔性航天器姿态机动的控制问题，给出了基于输出反馈的变结构跟踪控制算法。
The guidance method can meet the need of pinpoint soft landing, but its requirement for attitude change goes beyond the attitude maneuver capability of landing spacecraft.
该制导方法虽能满足精确软着陆的需要，但对姿态变化的要求超出了着陆器姿态机动能力。
This paper deals with the near-minimum-time attitude maneuver control of vertical launching tactical missile, in order to solve fast attitude maneuver of this kind of missile.
针对战术导弹垂直发射姿态调转时的快速性要求，研究了垂直发射快速姿态调转的次最小时间控制问题。
The designed maneuver reentry trajectory can meet the demands of attitude, heat flux and velocity for the warhead.
所设计的再入机动弹道能满足机动弹头对姿态、热流和速度的要求。
When tentatively applying the satire and the eulogy to express, it turns to the attitude and maneuver of the golden mean and mildness for helpand develop a creative way of "compromise" then.
它们在把握“讽刺”和“歌颂”性表现时，采取了中庸、平和的态度和策略，走出了一条“折衷”的创作路线。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
This method would be applied for the attitude capture and maneuvers control of the satellite at any time when the optimum maneuver trajectory was unknown.
在毋需获知最优机动轨迹规划的情况下，可用于卫星任意时刻的姿态捕获和机动控制。
When three baselines are used, during the maneuver of the vehicle, the baselines that are nearly orthogonal can estimate the attitude better than other frames of baselines.
当使用三基线的天线阵时，在飞行机动较大的情况下采用近似正交布局的天线结构可以更好地估计姿态。
In view of the particularity for maneuver warhead reentry trajectory and the guidance method, key techniques in attitude control system design are analyzed.
针对机动弹头再入弹道和制导方式的特殊性，分析了激光末制导机动弹头姿控系统设计的关键技术。
Assessing the accuracy of guidance system, especially controlling of missile's attitude and station keeping maneuver and landing point forecasting all rely on the reliable trajectory measurement.
飞行器制导精度评估，特别是航天器的姿态与定点控制、落点预报等，都离不开高精度的外弹道测量数据。
When the satellite takes orbital maneuver, the control force may stimulate the vibration of the flexible appendages and, therefore, affects the attitude of the satellite.
卫星轨道控制期间，轨道控制推力会激振挠性太阳帆板，从而也影响卫星的姿态。
The attitude control law is designed for the orbital maneuver with considering the output character of the attitude control thrusters.
根据姿态控制推力器的输出特性，设计了轨道控制期间卫星姿态控制方案。
The large angle maneuver is one of the key technologies for spacecraft attitude control, which has been the focus of attention.
大角度机动作为现代航天器姿态控制关键技术之一，一直为航天控制领域关注。
The large angle maneuver is one of the key technologies for spacecraft attitude control, which has been the focus of attention.
大角度机动作为现代航天器姿态控制关键技术之一，一直为航天控制领域关注。
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