Investigating the impact process between the hop** lander and the regolith surfaces is of
great significance for the in situ asteroid explorations. The high-efficiency description of the …

The problem investigated in this paper is how to rapidly optimize a landing trajectory on an
arbitrarily shaped asteroid, subject to practical constraints and a gravitational model suitable …

The aircraft four-dimensional trajectory planning is an important technology for multiple
aircraft to achieve cooperation. However, the current four-dimensional trajectory planning …

Taking into account the thruster performance (total thrust magnitude constraint and control
acceleration deviation) and glide-slope constraint, this paper presents two types of new …

This paper develops an autonomous flight control system to alleviate the heavy workload
involved in managing multiple emergencies during manned helicopter shipboard recovery …

During soft landing on asteroids, the weak gravity and rugged terrain put the spacecraft at
risk of crashing and bouncing, such that a safe and accurate landing is essential for the …

The guidance and control problem of spacecraft approaching an asteroid using constant
continuous thrust is studied in this work. The range of interest is from hundreds of kilometers …

Based on the application background of autonomous navigation for soft landing of small
celestial bodies, this paper proposes a robust navigation algorithm for the difficult problems …

Antes de que una nave espacial alcance una posición estacionaria sobre un asteroide para
realizar tareas orbitales, se deben realizar operaciones de proximidad. Dado que los …