China's Mars probe successfully completed its first orbital correction. /CCTV
The probe of China's first Mars mission, Tianwen-1, successfully carried out its first orbital correction Sunday morning, according to the China National Space Administration.
The probe completed the orbital correction at 7 a.m. Beijing time after its 3000N engine worked for 20 seconds.
It had flown for about 230 hours in space, traveling three million kilometers away from the Earth by the time of the first orbital correction.
All of its systems were in good condition.
The 3000N engine's performance in orbit was also verified at the same time as the orbital correction. Later, Tianwen-1 will undergo deep space maneuvers and several mid-course corrections before reaching Mars after a more than six-month flight.
China launched its first Mars mission Tianwen-1, which means "Questions to Heaven," on July 23, marking the country's first step in planetary exploration of the solar system.
The probe took a photo of the Earth and the Moon at a distance of 1.2 million kilometers away on Monday.
The probe will undergo deep space maneuvers and several mid-course corrections before reaching Mars. /CCTV
Why conduct orbital correction?
Similar to the lane keeping aid, known as LKA, for vehicles, orbital correction ensures the Mars probe travels along the planned orbit.
But the Mars probe has to correct not only the flight direction but also other variables, such as its flight speed. The probe also has no road markings as a reference in space, making the process much more difficult.
During the Earth-Mars transfer orbit, the probe will be affected by the deviation of orbit entry and control accuracy. As the flight is mostly unpowered and lasts a long time, the tiny inaccuracies in position and velocity will gradually accumulate, and cause the probe to miss the red planet if not corrected.
Therefore, a control strategy for mid-course orbital correction is indispensable, as it sets the time, speed increment and the direction of each correction.
Researchers for the flight mission need to conduct the corresponding attitude and orbital control of the probe according to the strategy to ensure that the probe always flies in the predetermined orbit.
The correction strategy will also be continually optimized according to the flight status of the probe.