Author: R. G. Walker
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 24
Book Description
Radiance measurements of the Earth's horizon in three infrared spectral regions were made during two Aerobee rocket flights at White Sands Missile Range, New Mexico. Preliminary results indicate equivalent blackbody radiation temperatures in the CO2 band (14.0 - 15.6 microns) varied from 231K to 239K; in the atmospheric window region (10.2 - 11.8 microns) from 205K to 287K; and in the rotational water vapor band (19.5 - 31.8 microns) from 206K to 239K. Numerous dropouts due to clouds are apparent in the atmospheric window and water vapor bands, while no such effect is evident in the CO2 band. The infrared radiometer, stellar aspect sensor and vehicle attitude control system are described, and actual traces of the horizon profiles and outputs from the stellar aspect system are included. (Author).
Measurement of the Infrared Horizon of the Earth
Author: R. G. Walker
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 24
Book Description
Radiance measurements of the Earth's horizon in three infrared spectral regions were made during two Aerobee rocket flights at White Sands Missile Range, New Mexico. Preliminary results indicate equivalent blackbody radiation temperatures in the CO2 band (14.0 - 15.6 microns) varied from 231K to 239K; in the atmospheric window region (10.2 - 11.8 microns) from 205K to 287K; and in the rotational water vapor band (19.5 - 31.8 microns) from 206K to 239K. Numerous dropouts due to clouds are apparent in the atmospheric window and water vapor bands, while no such effect is evident in the CO2 band. The infrared radiometer, stellar aspect sensor and vehicle attitude control system are described, and actual traces of the horizon profiles and outputs from the stellar aspect system are included. (Author).
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 24
Book Description
Radiance measurements of the Earth's horizon in three infrared spectral regions were made during two Aerobee rocket flights at White Sands Missile Range, New Mexico. Preliminary results indicate equivalent blackbody radiation temperatures in the CO2 band (14.0 - 15.6 microns) varied from 231K to 239K; in the atmospheric window region (10.2 - 11.8 microns) from 205K to 287K; and in the rotational water vapor band (19.5 - 31.8 microns) from 206K to 239K. Numerous dropouts due to clouds are apparent in the atmospheric window and water vapor bands, while no such effect is evident in the CO2 band. The infrared radiometer, stellar aspect sensor and vehicle attitude control system are described, and actual traces of the horizon profiles and outputs from the stellar aspect system are included. (Author).
Radiometric Measurements of the Earth's Infrared Horizon from the X-15 in Three Spectral Intervals
Author: Antony Jalink
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 66
Book Description
NASA Technical Note
Scientific and Technical Aerospace Reports
A Limb Radiance Calculation Approach for Model Atmospheres Containing Horizontal Gradients of Temperature and Pressure
Author: Richard E. Davis
Publisher:
ISBN:
Category : Atmospheric pressure
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Atmospheric pressure
Languages : en
Pages : 44
Book Description
Remote Sensing of Earth Resources
Author: NASA Scientific and Technical Information Facility
Publisher:
ISBN:
Category : Earth sciences
Languages : en
Pages : 620
Book Description
Publisher:
ISBN:
Category : Earth sciences
Languages : en
Pages : 620
Book Description
Air Force Research Resumés
Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods
Author: Yongchun Xie
Publisher: Springer Nature
ISBN: 9811569908
Category : Technology & Engineering
Languages : en
Pages : 495
Book Description
This book focuses on the theory and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). The position and attitude dynamics and kinematics equations for RVD are presented systematically in accordance with several different coordinate systems, including elliptical orbital frame, and recommendations are supplied on which of these equations to use in different phases of RVD. The book subsequently explains the basic principles and relative navigation algorithms of RVD sensors such as GNSS, radar, and camera-type RVD sensors. It also provides guidance algorithms and schemes for different phases of RVD, including the latest research advances in rapid RVD. In turn, the book presents a detailed introduction to intelligent adaptive control and proposes corresponding theoretical approaches to thruster configuration and control allocation for RVD. Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole. For purposes of verification, the Shenzhou spacecraft’s in-orbit flight mission is introduced as well. All issues addressed are described and explained from basic principles to detailed engineering methods and examples, providing aerospace engineers and students both a basic understanding of, and numerous practical engineering methods for, GNC system design in RVD.
Publisher: Springer Nature
ISBN: 9811569908
Category : Technology & Engineering
Languages : en
Pages : 495
Book Description
This book focuses on the theory and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). The position and attitude dynamics and kinematics equations for RVD are presented systematically in accordance with several different coordinate systems, including elliptical orbital frame, and recommendations are supplied on which of these equations to use in different phases of RVD. The book subsequently explains the basic principles and relative navigation algorithms of RVD sensors such as GNSS, radar, and camera-type RVD sensors. It also provides guidance algorithms and schemes for different phases of RVD, including the latest research advances in rapid RVD. In turn, the book presents a detailed introduction to intelligent adaptive control and proposes corresponding theoretical approaches to thruster configuration and control allocation for RVD. Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole. For purposes of verification, the Shenzhou spacecraft’s in-orbit flight mission is introduced as well. All issues addressed are described and explained from basic principles to detailed engineering methods and examples, providing aerospace engineers and students both a basic understanding of, and numerous practical engineering methods for, GNC system design in RVD.
Derivation and Statistical Comparison of Various Analytical Techniques which Define the Location of Reference Horizons in the Earth's Horizon Radiance Profile
Author: John R. Thomas
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 164
Book Description
Publisher:
ISBN:
Category : Infrared horizon sensors
Languages : en
Pages : 164
Book Description