Abstract
To achieve the goal of collecting lunar samples and return to the Earth for the Chang’E-5 spacecraft, the lander and ascender module (LAM) of the Chang’E-5 spacecraft successfully landed on the lunar surface on 1 Dec., 2020. The guidance, navigation, and control (GNC) system is one of the critical systems to perform this task. The GNC system of previous missions, Chang’E-3 and Chang’E-4, provides the baseline design for the Chang’E-5 LAM, and the new characteristics of the LAM, like larger mass and liquid sloshing, also bring new challenges for the GNC design. The GNC design for the descent and landing is presented in this paper. The guidance methods implemented in the powered descent are presented in detail for each phase. Propellant consumption and hazard avoidance should be particularly considered in the design. A reconfigurable attitude control is adopted which consists of the quaternion partition control, phase and gain stabilization filter, and dual observer. This controller could provide fast attitude maneuver and better system robustness. For the navigation, an intelligent heterogeneous sensor data fusion method is presented, and it is applied for the inertial measurement unit and velocimeter data. Finally, the flight results of the LAM are shown. Navigation sensors were able to provide valid measurement data during descent, and the thrusters and the main engine operated well as expected. Therefore, a successful soft lunar landing was achieved by the LAM.
Highlights
According to the Chang’E project plan [1], the mission objective of the Chang’E-5 spacecraft is to collect lunar surface samples and return to the Earth
The Chang’E-5 spacecraft consists of four vehicles: the orbiter, lander, ascender, and returner. These vehicles were launched as a combined module from the Earth, and the lander and ascender module (LAM) separated from the orbiter and returner module (ORM) in lunar orbit
The altitude went higher at the beginning of the trajectory since the powered descent began at the perilune point
Summary
According to the Chang’E project plan [1], the mission objective of the Chang’E-5 spacecraft is to collect lunar surface samples and return to the Earth. To achieve this mission, the Chang’E-5 spacecraft consists of four vehicles: the orbiter, lander, ascender, and returner. The returner alone carrying samples reentered into the Earth atmosphere and landed on the designated site In this way, the mission of Chang’E-5 is completed. To further reduce system weight, the landing and ascent functions of the GNC system are designed in sharing some sensors, attitude thrusters, and computing resources.
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