Add to ORKGPhase 1 of the Development of Autonomous Aerobraking (AA) Assessment investigated the technical capability of transferring the processes of aerobraking maneuver (ABM) decision-making (currently performed on the ground by an extensive workforce and communicated to the spacecraft via the deep space network) to an efficient flight software algorithm onboard the spacecraft. This document describes Phase 2 of this study, which was a 12-month effort to improve and rigorously test the AA Development Software developed in Phase 1. Aerobraking maneuver; Autonomous Aerobraking; Autonomous Aerobraking Development Software; Deep Space Network; NASA Engineering and Safety Cente
A multi-element study was done to assess the practicality of a Space Station Freedom-based aerobrake...
The integrated application of active controls (IAAC) technology to an advanced subsonic transport is...
An overview of the executive system design task is presented. The flight software executive system, ...
The NASA Engineering and Safety Center received a request from Mr. Daniel Murri (NASA Technical Fell...
NASA has used aerobraking at Mars and Venus to reduce the fuel required to deliver a spacecraft into...
The purpose of this flight test plan is to describe procedures for conducting FIM operations with th...
The Air Traffic Management Technology Demonstration-1 (ATD-1) is a major applied research and develo...
When entering orbit about a planet or moon with an appreciable atmosphere, instead of using only the...
Advanced capabilities planned for the next generation of aircraft, including those that will operate...
Two critical aspects of the Applications Engineering Program were especially successful: commerciali...
This paper describes an intelligent propulsion control architecture that coordinates with the flight...
This NASA Engineering and Safety Center (NESC) assessment was established to develop a set of time h...
The feasibility and practicality of employing an aerobraking trajectory for return of the reusable s...
Selected research and technology activities at NASA Dryden Flight Research Center are summarized. Th...
The costs to implement Autonomous Flight Rules (AFR) were examined for estimates in acquisition, ins...
A multi-element study was done to assess the practicality of a Space Station Freedom-based aerobrake...
The integrated application of active controls (IAAC) technology to an advanced subsonic transport is...
An overview of the executive system design task is presented. The flight software executive system, ...
The NASA Engineering and Safety Center received a request from Mr. Daniel Murri (NASA Technical Fell...
NASA has used aerobraking at Mars and Venus to reduce the fuel required to deliver a spacecraft into...
The purpose of this flight test plan is to describe procedures for conducting FIM operations with th...
The Air Traffic Management Technology Demonstration-1 (ATD-1) is a major applied research and develo...
When entering orbit about a planet or moon with an appreciable atmosphere, instead of using only the...
Advanced capabilities planned for the next generation of aircraft, including those that will operate...
Two critical aspects of the Applications Engineering Program were especially successful: commerciali...
This paper describes an intelligent propulsion control architecture that coordinates with the flight...
This NASA Engineering and Safety Center (NESC) assessment was established to develop a set of time h...
The feasibility and practicality of employing an aerobraking trajectory for return of the reusable s...
Selected research and technology activities at NASA Dryden Flight Research Center are summarized. Th...
The costs to implement Autonomous Flight Rules (AFR) were examined for estimates in acquisition, ins...
A multi-element study was done to assess the practicality of a Space Station Freedom-based aerobrake...
The integrated application of active controls (IAAC) technology to an advanced subsonic transport is...
An overview of the executive system design task is presented. The flight software executive system, ...