The level C software formulations requirements for the entry guidance and the simplified autopilot to be used by the Mission Control Center (MCC) entry processor are presented. The modifications required to functionally simulate optional Terminal Area Energy Management (TAEM) targeting capability (OTT) are incorporated. Implementation of this logic in the MCC must be coordinated with flight software OTT implementation and MCC TAEM guidance OTT. The entry guidance logic is based on the orbiter avionics entry guidance software. Descriptions of the entry guidance detailed formulation requirements, the detailed autopilot formulation requirements, and the targeting routine are given. Also included are a definition of coordinate systems, a list o...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The objective of this program is to develop generic load models with multiple levels of progressive ...
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...
Preliminary entry guidance and autopilot software formulations, for use in the Mission Control Cente...
An orbital maneuvering vehicle (OMV) front end kit is defined which is capable of performing in-situ...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Technical and management studies defining Apollo applications program payload integration task
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
Performance analysis and implementation of marine and air navigation and traffic control system usin...
In order to accommodate the rapid growth in commercial aviation throughout the remainder of this cen...
The EDIN (Engineering Design Integration) System which provides a collection of hardware and softwar...
A design and analysis study was conducted to provide advanced engine descriptions and parametric dat...
A general purpose FORTRAN program for simulating and optimizing point mass trajectories (POST) of ae...
The performance and economic benefits available by incorporation of advanced technologies into the s...
Final results of the Spaceflight Tracking and Data Network (STDN) Ranging Equipment program are summ...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The objective of this program is to develop generic load models with multiple levels of progressive ...
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...
Preliminary entry guidance and autopilot software formulations, for use in the Mission Control Cente...
An orbital maneuvering vehicle (OMV) front end kit is defined which is capable of performing in-situ...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Technical and management studies defining Apollo applications program payload integration task
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
Performance analysis and implementation of marine and air navigation and traffic control system usin...
In order to accommodate the rapid growth in commercial aviation throughout the remainder of this cen...
The EDIN (Engineering Design Integration) System which provides a collection of hardware and softwar...
A design and analysis study was conducted to provide advanced engine descriptions and parametric dat...
A general purpose FORTRAN program for simulating and optimizing point mass trajectories (POST) of ae...
The performance and economic benefits available by incorporation of advanced technologies into the s...
Final results of the Spaceflight Tracking and Data Network (STDN) Ranging Equipment program are summ...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The objective of this program is to develop generic load models with multiple levels of progressive ...
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...