The Mars atmospheric entry phase plays a vital role in the whole Mars exploration mission-
cycle. It largely determines the success of the entire Mars mission. In order to achieve a pin …

The nature of the bank angle modulation technique based on the low lift-to-drag
aerodynamic configuration of the entry vehicle inevitably introduces the problem of input …

Entry flight is a critical mission phase of planetary aeroassist problems. During atmospheric
flight, aleatory-epistemic uncertainty and environmental factors reduce the accuracy of …

With low-lifting capability taken into account, a robust guidance law for Mars entry vehicles
with low lift-to-drag ratios, such as Mars Science Laboratory (MSL), is presented. Consider …

Uncertainties present in the Mars atmospheric entry process may cause state deviations
from the nominal designed values, which will lead to unexpected performance degradation if …

Maximizing the terminal altitude for Mars atmospheric entry has long been investigated on
trajectory design to allow a sufficient timeline margin for subsequent operations and the …

ONE of the state-of-the-art entry technologies considered to significantly improve the
accuracy of Mars landing is the numerical predictor–corrector (NPC) guidance. There are …

The article deals with the aerothermodynamic and thermal analysis of two technological
demonstrators suitable for research activities on deployable heatshield entry capsules …

随着火星着陆探测任务的不断推进, 火星采样返回, 载人登火星和火星基地等任务要求能将更大,
更重的探测器着陆到火星表面, 这就需要在火星大气进入阶段进行高效减速 …

For improving landing accuracy on future Mars missions, robust entry guidance schemes are
required to improve landing accuracy. This paper analyzes the desensitized optimal …