navigation scheme造句
例句與造句
- as the navigation scheme
作為導航模式。 - vision-based autonomous landing integrated navigation scheme of unmanned combat aerial vehicles
基于視覺的無人作戰(zhàn)飛機自主著陸導航方案 - for the lunar landing phase mission, this paper presents autonomous navigation scheme based on feature points ( fps ) tracking
針對著陸軌道段任務,給出了一種基于特征點跟蹤的自主導航方法。 - construct a navigation scheme that is simple and intuitive . provide for pages anticipated . and even for the unexpected as possible
導航系統(tǒng)要簡單、直觀。既要考慮已預測的頁面,也要考慮未預測到的頁面。 - these are the best formats because surfers are accustomed to them . anything off these norms is liable to confuse . since confused visitors exit quickly, avoid unique or trick navigation schemes
用戶已經(jīng)習慣了這種格式,其它格式可能會迷惑用戶,導致用戶會退出網(wǎng)站。所以,避免出現(xiàn)獨特的導航系統(tǒng)。 - It's difficult to find navigation scheme in a sentence. 用navigation scheme造句挺難的
- in this thesis, the author gives a new navigation scheme for the flight vehicle : flight dynamics navigation method ( fdn ), and studies the principles of loading of digital map in the terrain auxiliary navigation
本文論證了一種具有創(chuàng)新性質(zhì)的導航方案??飛行力學導航法,并對地形輔助導航中數(shù)字地圖的加載問題進行了研究。 - secondly, based on the existing international technologic analysis, two different measurement schemes are proposed . one navigation scheme uses pixels as measurements vector, and the other one uses line of sight ( los ) of object celestial body and angles from probe to object body as the measurements vector
其次,通過對國際上現(xiàn)有技術(shù)的分析,給出兩種不同的導航觀測方案:一是利用圖像作為觀測量的自主導航;二是利用視線方向及夾角作為觀測量的自主導航。 - in deep space exploration missions, autonomous navigation technology is very important, and in this paper, we do some research into the autonomous navigation schemes of encountering small celestial bodies . it is mainly described as the follows : firstly, by analyzing the orbit characteristics and task requirements in encounter, the simplified orbit dynamic model for the deep space probe is built up, and whether the corresponding model error that meets the demanding of autonomous navigation task is validated
在深空探測任務中,自主導航技術(shù)是十分重要的,本文對交會小行星的自主導航方法進行研究,主要內(nèi)容包括:首先,分析交會小行星的軌道特性及任務需求,建立簡化的深空探測器軌道動力學模型,并驗證了簡化模型的誤差能否滿足自主導航任務的需求。 - finally, based on the observability analysis and error analysis, two autonomous navigation schemes for encounter phase are respectively proposed in detail . monte carlo simulations are done for the two schemes . by analyzing and comparing the simulation results, we can get the conclusion that, under the accuracy conditions provided by the instruments in existence, the position estimation accuracy for probe encountering object celestial body is 0.42km and 0.04km, which demonstrate the feasibility of the two navigation schemes
最后,在可觀性分析和誤差分析的基礎(chǔ)上,分別給出基于圖像測量的自主導航方法和基于視線方向及夾角測量的自主導航方法,并對這兩種方法進行蒙特卡羅數(shù)值仿真,通過對仿真結(jié)果的分析和比較,在現(xiàn)有儀器的測量精度下,探測器在與目標天體交會時刻的位置估計精度分別是0.42km和0.04km,由此表明兩種自主導航方案都是可行的。 - finally, based on the observability analysis and error analysis, two autonomous navigation schemes for encounter phase are respectively proposed in detail . monte carlo simulations are done for the two schemes . by analyzing and comparing the simulation results, we can get the conclusion that, under the accuracy conditions provided by the instruments in existence, the position estimation accuracy for probe encountering object celestial body is 0.42km and 0.04km, which demonstrate the feasibility of the two navigation schemes
最后,在可觀性分析和誤差分析的基礎(chǔ)上,分別給出基于圖像測量的自主導航方法和基于視線方向及夾角測量的自主導航方法,并對這兩種方法進行蒙特卡羅數(shù)值仿真,通過對仿真結(jié)果的分析和比較,在現(xiàn)有儀器的測量精度下,探測器在與目標天體交會時刻的位置估計精度分別是0.42km和0.04km,由此表明兩種自主導航方案都是可行的。