【祝融号的图像及科学数据传输必须依靠器间通信,故首批图像可能于今晚或明早回传】
有必要说明一下祝融号的通信与数据传输机制:
#祝融号#火星车设计了超高频(UHF)、X频段两种不同频率的数传链路。UHF链路作为主用数传链路,实现对环绕器的数据传输,数据率适中,但传输距离有限,只有当环绕器处于近火弧段时才能进行数传。出于简单方便考虑,UHF天线通常设计为固定天线,没有自主指向控制需求。
X频段链路采用可转动式定向天线,可以实现直接对地传输,但数据率太低,难以满足图像数据传输需求,通常用于应急状态;也可以实现对环绕器的数传,数据率相对较高,但存在天线指向控制需求,当环绕器位于近火弧段时,由于其方位角和高度角快速变化,对火星车定向天线提出了更高的指向控制要求。
根据这两种频段的特性,祝融号设计了两种通信数传机制:一是X频段直接对地通信,二是器间通信(UHF为主,X频段为辅)。
1.X频段直接对地通信:持续时间长,但数传速率极低,仅为16bps,故主要用于传输工程遥测数据以供判断火星车状态,传输图像啥的是不可能的。
2.器间通信(UHF为主,X频段为辅):持续时间短,但数传速率较高,主要用于传输图像及科学探测数据。环绕器在中继通信轨道运行期间,祝融号每一个火星日(sol)可与处在近火弧段的环绕器进行一次器间UHF双向通信,每次约8~10min,平均数传速率约38kbps,平均数传量20Mbit;受供电约束影响,每3sol才能与处在远火弧段的环绕器进行一次器间X频段通信(单向,只可发送),每次约25min,数传速率约32kbps,数传量约50Mbit。
5月15日7时许,祝融号落火,此后的环绕器在265×65000km×86.9º(轨道周期2sol)的停泊轨道上又飞行1圈。
5月17日(今天)早上8:15左右,环绕器至近火点,进行第四次近火制动,随后进入265×15000km×86.9º(轨道周期1/3sol)的中继通信轨道。
故在此之前,一直使用X频段直接对地通信的祝融号,其数传下行速率只有16bps(2字节/s),不可能传输得了图像。
在此之后,它将每个sol绕飞火星3圈,则每个sol都有一次近火弧段UHF器间通信窗口,也都有一次X频段远火弧段通信窗口,且相邻的近火弧段通信窗口与远火弧段通信窗口间隔为1/2sol。
参考资料:彭松,尺清,郑旸.火星车自主功能方案设计[J].国际太空,2020(07):14-18.
PhilLeafSpace
Today at 07:44 from HUAWEI P30 Pro Edited
[Zhurong’s image and scientific data transmission must rely on inter-device communication, so the first batch of images may be returned tonight or tomorrow morning]
It is necessary to explain the communication and data transmission mechanism of Zhurong:
The Mars Rover Zhurong has designed two data transmission links of ultra-high frequency (UHF) and X-band at two different frequencies. UHF link is used as the main data transmission link to realize data transmission to surround device. The data rate is moderate, and the transmission distance is limited. Data transmission can only be carried out when the surround device is in the periareion arc. For the sake of simplicity and convenience, UHF antennas are usually designed as fixed antennas, and there is no need for autonomous pointing control. The X-band link uses a rotatable directional antenna, which can realize direct-to-earth transmission, but the data rate is too low to meet the demand for image data transmission and is usually used in emergency situations; Data transmission to the orbiter can also be realized. The data rate is relatively high, but there is a need for antenna pointing control. When the orbiter is located in the periareion arc, due to the rapid change of its azimuth and altitude angles, a directional antenna for the Mars rover is required with higher pointing control capability.
Based on the characteristics of these two frequency bands, Zhurong has designed two communication data transmission mechanisms: one is X-band direct-to-earth communication, and the other is inter-device communication (UHF is the main and X-band is the secondary).
1. X-band direct-to-earth communication: duration is long, but the data transmission rate is very low, only 16bps, so it is mainly used to transmit engineering telemetry data on the status of the rover. It is impractical to transmit images.
2. Inter-device communication (UHF as main, X frequency band as auxiliary): short duration, but higher data transmission rate, mainly used to transmit images and scientific data. When the orbiter is in the relay communication orbit, Zhurong can perform UHF two-way communication with the orbiter in the periareion arc on each Martian day (sol), each time about 8-10 minutes, and the average data transmission rate is about 38kbps, the average data transmission capacity is 20Mbit; affected by power supply constraints, inter-device X-band communication (one-way, only sending) can be performed with the surround device in apoareion arc section every 3sol, and the data transmission rate is about 25min each time. Rate is about 32kbps, the data transmission capacity is about 50Mbit.
At about 7 o'clock on May 15th, Zhurong begin landing on Mars, after which the orbiter flew one more circle on the parking orbit of 265×65000km×86.9º (orbital period 2sol). At around 8:15 in the morning of May 17 (today), the orbiter reached the periareion point for the fourth periareion braking, and then entered the relay communication orbit of 265×15000km×86.9º (orbital period 1/3sol).
Therefore, before this, the ZhuRong rover, which has been using the X frequency band to communicate directly to earth, has a data transmission downlink rate of only 16 bps (2 bytes/s), and it is impossible to transmit images. After that, it will fly 3 times around Mars each sol, then each sol will have a periareion arc UHF communication window, and a X-band apoareion arc communication window. The interval between periareion and apoareion communication window is 1/2 sol.
According to this calculation, the first X-band communication window for the apoareion arc is around 20:30 on May 17, and the first UHF periareion arc communication window is around 8:50 on the morning of May 18. Zhurong may return the Mars images acquired during these two time windows. The communication window on the morning of May 18 is also in line with the stated plan that "UHF Inter-device communication link will be established after 3 sols".
@China Air Force @Steed的围铃 @haibaraemily @航空物语 @NASAenthusiast
Reference materials: Peng Song, Chi Qing, Zheng Yang. The design of the autonomous function scheme of the Mars rover[J].International Space,2020(07):14-18.