Review and prospect of guidance and control for Mars atmospheric entry

S Li, X Jiang - Progress in Aerospace Sciences, 2014 - Elsevier
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 …

Mars entry, descent, and landing instrumentation 2 trajectory, aerodynamics, and atmosphere reconstruction

CD Karlgaard, M Schoenenberger, S Dutta… - Journal of Spacecraft …, 2023 - arc.aiaa.org
On February 18th, 2021, the Mars 2020 entry system successfully delivered the
Perseverance rover to the surface of Mars at Jezero Crater. The entry capsule carried a set …

Mars 2020 entry, descent, and landing system overview

A Nelessen, C Sackier, I Clark… - 2019 IEEE …, 2019 - ieeexplore.ieee.org
Building upon the success of the Mars Science Laboratory (MSL) landing and surface
mission, the Mars 2020 project is a flagship-class science mission intended to address key …

Aerothermal measurements from the ExoMars Schiaparelli capsule entry

A Gülhan, T Thiele, F Siebe, R Kronen… - Journal of Spacecraft …, 2019 - arc.aiaa.org
The instrumentation package COMARS+ was developed to measure aerothermal
parameters on the back cover of the ExoMars Schiaparelli lander during Martian entry. The …

Preliminary assessment of the Mars Science Laboratory entry, descent, and landing simulation

DW Way - 2013 IEEE Aerospace Conference, 2013 - ieeexplore.ieee.org
On August 5, 2012, the Mars Science Laboratory rover, Curiosity, successfully landed inside
Gale Crater. This landing was the seventh successful landing and fourth rover to be …

Mars science laboratory entry atmospheric data system trajectory and atmosphere reconstruction

CD Karlgaard, P Kutty, M Schoenenberger… - Journal of Spacecraft …, 2014 - arc.aiaa.org
On 5 August 2012, the Mars Science Laboratory entry vehicle successfully entered Mars's
atmosphere and landed the Curiosity rover on its surface. The entry vehicle carried a system …

Feasibility and performance analysis of neptune aerocapture using heritage blunt-body aeroshells

AP Girija, SJ Saikia, JM Longuski… - Journal of Spacecraft …, 2020 - arc.aiaa.org
Large navigation and atmospheric uncertainties have historically driven the need for a mid-
lift-to-drag-ratio (mid-L/D) vehicle with (L/D) max of 0.6–0.8 for aerocapture at Neptune. Most …

Adaptable deployable entry and placement technology sounding rocket one modeling and reconstruction

S Dutta, CD Karlgaard, AM Korzun, JS Green… - Journal of Spacecraft …, 2022 - arc.aiaa.org
Sounding Rocket One (SR-1), the first flight test of the Adaptable Deployable Entry and
Placement Technology (ADEPT), was performed on September 12, 2018. ADEPT is a …

Uranus Flagship-class Orbiter and Probe Using Aerocapture

S Dutta, E Shellabarger, JB Scoggins… - AIAA SciTech 2024 …, 2024 - arc.aiaa.org
The 2022 Planetary Science Decadal Survey released by the National Academies of
Science identified the exploration of the Ice Giants, particularly Uranus, as the primary next …

RBF neural network based second-order sliding mode guidance for Mars entry under uncertainties

S Li, X Jiang - Aerospace Science and Technology, 2015 - Elsevier
There are usually larger uncertainties in the atmosphere density of Mars and the
aerodynamic parameters of entry vehicles, which inevitably degrades the performance of …